HR job title
- Distinguished Professor
- Contact Info
- 1 979 845 3738
- Websites
Han, Je-Chin Distinguished Professor
Positions
- Distinguished Professor, Mechanical Engineering, College of Engineering
- Faculty Affiliate, Energy Institute, Texas A&M Engineering Experiment Station (TEES)
My research focuses on thermal Fluid Sciences - heat transfer and cooling in gas turbines, heat transfer enhancement, heat transfer in rotating flows, film cooling in unsteady high turbulent flows, combustor-liner cooling, mini-channel heat transfer, advanced CFD and experimental methods.
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- Publications
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- Works By Students
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Overview
Publications
selected publications
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academic article
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Alsaleem, S. M., Wright, L. M., & Han, J.
(2021).
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations. Journal of Turbomachinery.
143(9),
-
Wright, L. M., Chen, A. F., Wu, H., Han, J., Lee, C., Azad, S., & Um, J.
(2021).
Heat Transfer Enhancement in a Rectangular Cooling Channel With Airfoil Shaped Fins. Journal of Thermal Science and Engineering Applications.
13(4),
-
Chen, I., Sahin, I., Wright, L. M., Han, J., & Krewinkel, R.
(2021).
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs. Journal of Turbomachinery.
143(8),
-
Sahin, I., Chen, I., Wright, L. M., Han, J., Xu, H., & Fox, M.
(2021).
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins. Journal of Turbomachinery.
143(7),
-
Sahin, I., Chen, I., Wright, L. M., Han, J., Xu, H., & Fox, M.
(2021).
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins. Journal of Turbomachinery.
143(6),
-
Salinas, D. A., Ullah, I., Wright, L. M., Han, J., McClintic, J. W., Crites, D. C., & Riahi, A.
(2021).
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade. Journal of Turbomachinery.
143(6),
-
Shiau, C., Sahin, I., Ullah, I., Han, J., Mirzamoghadam, A. V., Riahi, A., & Stimpson, C.
(2020).
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique. Journal of Turbomachinery.
142(8),
-
Sahin, I., Chen, A. F., Shiau, C., Han, J., & Krewinkel, R.
(2020).
Effect of 45-deg Rib Orientations on Heat Transfer in a Rotating Two-Pass Channel With Aspect Ratio from 4:1 to 2:1. Journal of Turbomachinery.
142(7),
-
Shiau, C., Chen, A. F., Han, J., & Krewinkel, R.
(2020).
Detailed Heat Transfer Coefficient Measurements on a Scaled Realistic Turbine Blade Internal Cooling System. Journal of Thermal Science and Engineering Applications.
12(3),
-
Nuntakulamarat, M., Shiau, C., & Han, J.
(2020).
Heat Transfer and Pressure Drop Measurements in a High Aspect Ratio Channel With Circular Pins and Strip Fins. Journal of Thermal Science and Engineering Applications.
12(3), 1-28.
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Wright, L. M., Yang, S., Wu, H., Han, J., Lee, C., Azad, S., & Um, J.
(2020).
Heat Transfer in a Rotating, Blade-Shaped Serpentine Cooling Passage With Discrete Ribbed Walls at High Reynolds Numbers. Journal of Heat Transfer.
142(1),
-
Chen, A. F., Shiau, C., Han, J., & Krewinkel, R.
(2019).
Heat Transfer in a Rotating Two-Pass Rectangular Channel Featuring a Converging Tip Turn With Various 45 deg Rib Coverage Designs. Journal of Thermal Science and Engineering Applications.
11(6),
-
Faghri, M., Amano, R., Cheng, P., Chiu, W., Djilali, N., Ekkad, S., ... Zhao, T.
(2019).
Professor Bengt Sunden on his 70th Birthday. International Journal of Heat and Mass Transfer.
141, 1315-1317.
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Zhang, M., Wang, N., & Han, J.
(2019).
Internal heat transfer of film-cooled leading edge model with normal and tangential impinging jets. International Journal of Heat and Mass Transfer.
139, 193-204.
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Zhang, M., Wang, N., & Han, J.
(2019).
Overall effectiveness of film-cooled leading edge model with normal and tangential impinging jets. International Journal of Heat and Mass Transfer.
139, 577-587.
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Chen, A. F., Shiau, C., Han, J., & Krewinkel, R.
(2019).
Heat Transfer in a Rotating Two-Pass Rectangular Channel Featuring Reduced Cross-Sectional Area After Tip Turn (Aspect Ratio=4:1 to 2:1) With Profiled 60 deg Angled Ribs. Journal of Turbomachinery.
141(7), 1-40.
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Ullah, I., Shiau, C., & Han, J.
(2019).
Flat plate film cooling with linear and curved round-to-diffusion shaped slots using PSP measurement technique. 136, 755-766.
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Wang, N., & Han, J.
(2019).
Swirl Impinging Cooling on an Airfoil Leading Edge Model at Large Reynolds Number. Journal of Thermal Science and Engineering Applications.
11(3),
-
Shiau, C., Sahin, I., Wang, N., Han, J., Xu, H., & Fox, M.
(2019).
Turbine Vane Endwall Film Cooling Comparison From Five Film-Hole Design Patterns and Three Upstream Injection Angles. Journal of Thermal Science and Engineering Applications.
11(3),
-
Wang, N., Zhang, M., Shiau, C., & Han, J.
(2019).
Film Cooling Effectiveness From Two Rows of Compound Angled Cylindrical Holes Using Pressure-Sensitive Paint Technique. Journal of Heat Transfer.
141(4), 042202.
-
Wang, N., Shiau, C., Han, J., Xu, H., & Fox, M.
(2019).
Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection. International Journal of Heat and Mass Transfer.
133, 247-255.
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Wang, N., Zhang, M., Alsaleem, S., Wright, L. M., & Han, J.
(2019).
TURBINE BLADE LEADING EDGE IMPINGEMENT COOLING FROM NORMAL OR TANGENTIAL JETS WITH CROSSFLOW EFFECT. Frontiers in Heat and Mass Transfer.
13.
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Han, J.
(2018).
Advanced Cooling in Gas Turbines 2016 Max Jakob Memorial Award Paper. Journal of Heat Transfer.
140(11),
-
Shiau, C., Chowdhury, N., Han, J., Mirzamoghadam, A. V., & Riahi, A.
(2018).
Transonic Turbine-Vane Film Cooling with Showerhead Effect Using Pressure-Sensitive Paint Measurement Technique. Journal of Thermophysics and Heat Transfer.
32(3), 637-647.
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Chen, A. F., Wu, H., Wang, N., & Han, J.
(2018).
Heat Transfer in a Rotating Cooling Channel (AR=2:1) With Rib Turbulators and a Tip Turning Vane. Journal of Heat Transfer.
140(10),
-
Wang, N., Chen, A. F., Zhang, M., & Han, J.
(2018).
Turbine Blade Leading Edge Cooling With One Row of Normal or Tangential Impinging Jets. Journal of Heat Transfer.
140(6),
-
Wu, H., Zirakzadeh, H., Han, J., Zhang, L., & Moon, H.
(2018).
Heat Transfer in a Rib and Pin Roughened Rotating Multipass Channel With Hub Turning Vane and Trailing-Edge Slot Ejection. Journal of Thermal Science and Engineering Applications.
10(2), 021011.
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Shiau, C., Chen, A. F., Han, J., Azad, S., & Lee, C.
(2018).
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique. Journal of Turbomachinery.
140(2),
-
Chu, H., Chen, H., & Han, J.
(2018).
Numerical Simulation of Flow and Heat Transfer in Rotating Cooling Passage With Turning Vane in Hub Region. Journal of Heat Transfer.
140(2), 021701.
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Chen, A. F., Shiau, C., & Han, J.
(2018).
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions. Journal of Turbomachinery.
140(1), 011006.
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Bashir, M. H., Shiau, C., & Han, J.
(2017).
Film cooling effectiveness for three-row compound angle hole design on flat plate using PSP technique. 115, 918-929.
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Chowdhury, N., Qureshi, S. A., Zhang, M., & Han, J.
(2017).
Influence of turbine blade leading edge shape on film cooling with cylindrical holes. International Journal of Heat and Mass Transfer.
115, 895-908.
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Chowdhury, N., Zirakzadeh, H., & Han, J.
(2017).
A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis. Journal of Turbomachinery.
139(9), 091010.
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Yang, S., Wu, H., Han, J., Zhang, L., & Moon, H.
(2017).
Heat transfer in a smooth rotating multi-passage channel with hub turning vane and trailing-edge slot ejection. International Journal of Heat and Mass Transfer.
109, 1-15.
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Chowdhury, N., Shiau, C., Han, J., Zhang, L., & Moon, H.
(2017).
Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration. Journal of Turbomachinery.
139(6), 061003.
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Chen, A. F., Shiau, C., & Han, J.
(2017).
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions. Journal of Turbomachinery.
139(3), 031012.
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Ekkad, S. V., & Han, J. C.
(2017).
A transient liquid crystal image technique for local heat transfer distributions near a sharp 180 turn of a two-pass smooth square channel. Journal of Flow Visualization and Image Processing.
24(1-4), 127-140.
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Han, J., Huang, J. J., & Lee, C. P.
(2017).
Heat Transfer in Square Channels with Wedge-Shaped and Delta-Shaped Turbulence Promoters. Journal of Enhanced Heat Transfer.
24(1-6), 101-116.
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Zhang, Y. M., Han, J. C., & Lee, C. P.
(2017).
Turbulent Flow in Circular Tubes with Twisted-Tape Inserts and Axial Interrupted Ribs. Journal of Enhanced Heat Transfer.
24(1-6), 243-254.
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Li, S., Yang, S., Han, J., Zhang, L., & Moon, H.
(2016).
Turbine Blade Surface Phantom Cooling from Upstream Nozzle Trailing-Edge Ejection. 30(4), 770-781.
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Li, S., Lee, J., Han, J., Zhang, L., & Moon, H.
(2016).
Turbine Platform Cooling and Blade Suction Surface Phantom Cooling From Simulated Swirl Purge Flow. Journal of Turbomachinery.
138(8), 081004.
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Shiau, C., Chen, A. F., Han, J., Azad, S., & Lee, C.
(2016).
Full-Scale Turbine Vane Endwall Film-Cooling Effectiveness Distribution Using Pressure-Sensitive Paint Technique. 138(5), 051002.
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Li, S., Lee, J., Han, J., Zhang, L., & Moon, H.
(2016).
Influence of mainstream turbulence on turbine blade platform cooling from simulated swirl purge flow. Applied Thermal Engineering.
101, 678-685.
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Chen, A. F., Li, S., & Han, J.
(2015).
Film Cooling for Cylindrical and Fan-Shaped Holes Using Pressure-Sensitive Paint Measurement Technique. 29(4), 775-784.
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Ekkad, S., & Han, J.
(2015).
A REVIEW OF HOLE GEOMETRY AND COOLANT DENSITY EFFECT ON FILM COOLING. Frontiers in Heat and Mass Transfer.
6(1),
-
Rezasoltani, M., Lu, K., Schobeiri, M. T., & Han, J.
(2015).
A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition. Journal of Turbomachinery.
137(5), 051009.
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Yang, S., Han, J., Azad, S., & Lee, C.
(2015).
Heat Transfer in Rotating Serpentine Coolant Passage With Ribbed Walls at Low Mach Numbers. Journal of Thermal Science and Engineering Applications.
7(1), 011013.
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Mhetras, S., Han, J., & Huth, M.
(2014).
Heat Transfer and Pressure Loss Measurements in a Turbulated High Aspect Ratio Channel With Large Reynolds Number Flows. 6(4), 041001.
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Liu, K., Yang, S., & Han, J.
(2014).
Influence of Coolant Density on Turbine Platform Film-Cooling With Stator-Rotor Purge Flow and Compound-Angle Holes. 6(4), 041007.
-
Lee, M. S., Jeong, S. S., Ahn, S. W., & Han, J. C.
(2014).
Effects of angled ribs on turbulent heat transfer and friction factors in a rectangular divergent channel. International Journal of Thermal Sciences.
84, 1-8.
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Rezasoltani, M., Schobeiri, M. T., & Han, J. C.
(2014).
Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine With Nonaxisymmetric End Wall Contouring. Journal of Turbomachinery.
136(9), 091009.
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Rallabandi, A., Lei, J., Han, J., Azad, S., & Lee, C.
(2014).
Heat Transfer Measurements in Rotating Blade–Shape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers. Journal of Turbomachinery.
136(9), 091004.
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Lei, J., Li, S., Han, J., Zhang, L., & Moon, H.
(2014).
Effect of a Turning Vane on Heat Transfer in Rotating Multipass Rectangular Smooth Channel. 28(3), 417-427.
-
Mhetras, S., Han, J., & Huth, M.
(2014).
Impingement Heat Transfer From Jet Arrays on Turbulated Target Walls at Large Reynolds Numbers. 6(2), 021003.
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Li, S., Yang, S., & Han, J.
(2014).
Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique. Journal of Turbomachinery.
136(5), 051011.
-
Liu, K., Yang, S., & Han, J.
(2014).
Influence of Coolant Density on Turbine Blade Film-Cooling With Axial and Compound Shaped Holes. 136(4), 044501.
-
Wright, L. M., & Han, J.
(2014).
HEAT TRANSFER ENHANCEMENT FOR TURBINE BLADE INTERNAL COOLING. 21(2-3), 111-140.
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Lee, M. S., Jeong, S. S., Ahn, S. W., & Han, J. C.
(2013).
Heat Transfer and Friction in Rectangular Convergent and Divergent Channels with Ribs. Journal of Thermophysics and Heat Transfer.
27(4), 660-667.
-
Han, J.
(2013).
Fundamental Gas Turbine Heat Transfer. 5(2), 021007.
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Lei, J., Li, S., Han, J., Zhang, L., & Moon, H.
(2013).
Heat Transfer in Rotating Multipass Rectangular Ribbed Channel With and Without a Turning Vane. 135(4), 041903.
-
Gao, Z., Rhee, D. H., & Han, J. C.
(2013).
Turbine Blade Trailing Edge Film Cooling Using PSP Technique. 13(3), 193-205.
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Li, S., Rallabandi, A. P., & Han, J.
(2012).
INFLUENCE OF UNSTEADY WAKE WITH TRAILING EDGE COOLANT EJECTION ON TURBINE BLADE FILM COOLING. Journal of Turbomachinery.
134(6), 435-445.
-
Lei, J., Han, J., & Huh, M.
(2012).
Effect of Rib Spacing on Heat Transfer in a Two Pass Rectangular Channel (AR=2:1) at High Rotation Numbers. Journal of Heat Transfer.
134(9), 091901.
-
Rallabandi, A. P., Li, S., & Han, J.
(2012).
Unsteady Wake and Coolant Density Effects on Turbine Blade Film Cooling Using Pressure Sensitive Paint Technique. Journal of Heat Transfer.
134(8), 081701.
-
Narzary, D. P., Liu, K., Rallabandi, A. P., & Han, J.
(2012).
Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique. 134(3), 031006-509.
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Montomoli, F., Massini, M., Yang, H., & Han, J. C.
(2012).
The benefit of high-conductivity materials in film cooled turbine nozzles. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW.
34, 107-116.
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Liu, Y., Huh, M., & Han, J.
(2012).
High rotation number effect on heat transfer in a trailing edge channel with tapered ribs. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW.
33(1), 182-192.
-
Mhetras, S., Han, J., & Rudolph, R.
(2012).
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade. 134(1), 011004.
-
Huh, M., Lei, J., & Han, J.
(2012).
Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers. Journal of Turbomachinery.
134(1), 011022.
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Gao, Z., Narzary, D. P., Mhetras, S., & Han, J. C.
(2012).
Upstream Vortex Effect on Turbine Platform Film Cooling with Typical Purge Flow. Journal of Thermophysics and Heat Transfer.
26(1), 75-84.
-
Rallabandi, A. P., Grizzle, J., & Han, J.
(2011).
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP. 133(4), 041024.
-
Alkhamis, N. Y., Rallabandi, A. P., & Han, J.
(2011).
Heat Transfer and Pressure Drop Correlations for Square Channels With V-Shaped Ribs at High Reynolds Numbers. Journal of Heat Transfer.
133(11), 111901.
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Rallabandi, A. P., Alkhamis, N., & Han, J.
(2011).
Heat Transfer and Pressure Drop Measurements for a Square Channel With 45 deg Round-Edged Ribs at High Reynolds Numbers. 133(3), 031019.
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Huh, M., Lei, J., Liu, Y., & Han, J.
(2011).
High Rotation Number Effects on Heat Transfer in a Rectangular (AR=2:1) Two-Pass Channel. Journal of Turbomachinery.
133(2), 021001.
-
Han, J., & Rallabandi, A. P.
(2010).
TURBINE BLADE FILM COOLING USING PSP TECHNIQUE. Frontiers in Heat and Mass Transfer.
1(1),
-
Suryanarayanan, A., Ozturk, B., Schobeiri, M. T., & Han, J. C.
(2010).
Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique. Journal of Turbomachinery.
132(4), 041001-13.
-
Rallabandi, A. P., Rhee, D., Gao, Z., & Han, J.
(2010).
Heat transfer enhancement in rectangular channels with axial ribs or porous foam under through flow and impinging jet conditions. International Journal of Heat and Mass Transfer.
53(21-22), 4663-4671.
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Liu, Y., Huh, M., Han, J., & Moon, H.
(2010).
High Rotation Number Effect on Heat Transfer in a Triangular Channel With 45 deg, Inverted 45 deg, and 90 deg Ribs. 132(7), 071702-10.
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Narzary, D. P., Liu, K., Rallabandi, A. P., & Han, J.
(2010).
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING USING PRESSURE SENSITIVE PAINT TECHNIQUE. Journal of Turbomachinery.
134(3), 1529-1540.
-
Liu, Y., Huh, M., Rhee, D., Han, J., & Moon, H.
(2009).
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation Numbers. 131(4), 041017-12.
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Yang, H., Gao, Z., Chen, H. C., Han, J. C., & Schobeir, M. T.
(2009).
Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1-1/2 Turbine Stage. 131(4), 041003-12.
-
Gao, Z., Narzary, D., & Han, J.
(2009).
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling. Journal of Turbomachinery.
131(4), 041004-11.
-
Huh, M., Liu, Y., & Han, J.
(2009).
Effect of rib height on heat transfer in a two pass rectangular channel (AR=1:4) with a sharp entrance at high rotation numbers. International Journal of Heat and Mass Transfer.
52(19-20), 4635-4649.
-
Gao, Z., Narzary, D., Mhetras, S., & Han, J.
(2009).
Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling. Journal of Turbomachinery.
131(3), 031005.
-
Rallabandi, A. P., Yang, H., & Han, J.
(2009).
Heat Transfer and Pressure Drop Correlations for Square Channels With 45 Deg Ribs at High Reynolds Numbers. 131(7), 071703-10.
-
Narzary, D. P., Liu, K., & Han, J.
(2009).
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE PLATFORM FILM-COOLING. Journal of Thermal Science and Engineering Applications.
4(2), 287-299.
-
Gao, Z., & Han, J.
(2009).
Influence of Film-Hole Shape and Angle on Showerhead Film Cooling Using PSP Technique. Journal of Heat Transfer.
131(6), 061701-11.
-
Wright, L. M., Blake, S. A., Rhee, D., & Han, J.
(2009).
Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow. Journal of Turbomachinery.
131(2), 021017.
-
Liu, Y., Huh, M., Wright, L. M., & Han, J.
(2009).
Heat Transfer in Trailing-Edge Channels with Slot Ejection Under High Rotation Numbers. Journal of Thermophysics and Heat Transfer.
23(2), 305-315.
-
Huh, M., Liu, Y., Han, J., & Chopra, S.
(2009).
Rib-Spacing Effect on Heat Transfer in Rectangular Channels at High Rotation Numbers. Journal of Thermophysics and Heat Transfer.
23(2), 294-304.
-
Suryanarayanan, A., Mhetras, S. P., Schobeiri, M. T., & Han, J. C.
(2009).
Film-Cooling Effectiveness on a Rotating Blade Platform. Journal of Turbomachinery.
131(1), 011014.
-
Gao, Z., Narzary, D. P., & Han, J.
(2009).
Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes. 131(1), 011019.
-
Liu, Y., Huh, M., Han, J., & Chopra, S.
(2008).
Heat transfer in a two-pass rectangular channel (AR=1 : 4) under high rotation numbers. Journal of Heat Transfer.
130(8), 081701.
-
Wright, L. M., Gao, Z., Yang, H., & Han, J.
(2008).
Film cooling effectiveness distribution on a gas turbine blade platform with inclined slot leakage and discrete film hole flows. Journal of Heat Transfer.
130(7), 071702.
-
Wright, L. M., Liu, Y., Han, J., & Chopra, S.
(2008).
Heat transfer in trailing edge, wedge-shaped cooling channels under high rotation numbers. 130(7), 071701.
-
Liu, Y., Huh, M., Wright, L. M., & Han, J.
(2008).
Heat Transfer in Trailing Edge, Wedge Shaped Cooling Channels with Slot Ejection under High Rotation Numbers. Journal of Thermal Science and Engineering Applications.
3(2), 311-320.
-
Yang, H., Chen, H., Han, J., & Moon, H.
(2008).
Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage. International Journal of Heat and Mass Transfer.
51(11-12), 3066-3081.
-
Gao, Z., Narzary, D. P., & Han, J.
(2008).
Film cooling on a gas turbine blade pressure side or suction side with axial shaped holes. International Journal of Heat and Mass Transfer.
51(9-10), 2139-2152.
-
Mhetras, S., Narzary, D., Gao, Z., & Han, J. C.
(2008).
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip. Journal of Turbomachinery.
130(2),
-
Yang, H., Chen, H., Han, J., & Moon, H.
(2008).
Film-cooling prediction on rotor blade leading edge in 1-1/2 turbine stage. Journal of Thermophysics and Heat Transfer.
22(2), 201-209.
-
Choi, J., Mhetras, S., Han, J., Lau, S. C., & Rudolph, R.
(2008).
Film cooling and heat transfer on two cutback trailing edge models with internal perforated blockages. Journal of Heat Transfer.
130(1), 012201.
-
Liu, Y., Wright, L. M., Fu, W., & Han, J.
(2007).
Rib spacing effect on heat transfer in rotating two-pass ribbed channel (AR=1:2). Journal of Thermophysics and Heat Transfer.
21(3), 582-595.
-
Su, G., Chen, H., & Han, J.
(2007).
Computation of flow and heat transfer in rotating rectangular channels (AR=4 : 1) with pin-fins by a Reynolds stress turbulence model. Journal of Heat Transfer.
129(6), 685-696.
-
Ahn, J., Schobeiri, M. T., Han, J., & Moon, H.
(2007).
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes. International Journal of Heat and Mass Transfer.
50(1-2), 15-25.
-
Ahn, J., Schobeiri, M. T., Han, J., & Moon, H.
(2006).
Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint. Journal of Heat Transfer.
128(9), 879-888.
-
Mhetras, S., Yang, H., Gao, Z., & Han, J.
(2006).
Film-cooling effectiveness on squealer cavity and rim walls of gas-turbine blade tip. Journal of Propulsion and Power.
22(4), 889-899.
-
Yang, H., Chen, H., & Han, J.
(2006).
Film-cooling prediction on turbine blade tip with various film hole configurations. Journal of Thermophysics and Heat Transfer.
20(3), 558-568.
-
Fu, W., Wright, L. M., & Han, J.
(2006).
Heat transfer in two-pass rotating rectangular channels (AR=2:1) with discrete ribs. Journal of Thermophysics and Heat Transfer.
20(3), 569-582.
-
Han, J. C.
(2006).
Turbine blade cooling studies at Texas A&M University: 1980-2004. Journal of Thermophysics and Heat Transfer.
20(2), 161-187.
-
Han, J. C., & Chen, H. C.
(2006).
Turbine blade internal cooling passages with rib turbulators. Journal of Propulsion and Power.
22(2), 226-248.
-
Ahn, J., Mhetras, S., & Han, J. C.
(2005).
Film-cooling effectiveness on a gas turbine blade tip using pressure-sensitive paint. Journal of Heat Transfer.
127(5), 521-530.
-
Wright, L. M., Fu, W. L., & Han, J. C.
(2005).
Influence of entrance geometry on heat transfer in rotating rectangular cooling channels (AR=4:1) with angled ribs. Journal of Heat Transfer.
127(4), 378-387.
-
Parsons, J. A., & Han, J. C.
(2005).
Jet-impingement heat transfer in rotating channels with staggered extraction flow. Journal of Thermophysics and Heat Transfer.
19(2), 156-162.
-
Fu, W., Wright, L. M., & Han, J.
(2005).
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With Smooth Walls. Journal of Heat Transfer.
127(3), 265-277.
-
Lee, E., Wright, L. M., & Han, J. C.
(2005).
Heat transfer in rotating rectangular channels with V-shaped and angled ribs. Journal of Thermophysics and Heat Transfer.
19(1), 48-56.
-
Al-Qahtani, M., Chen, H. C., & Han, J. C.
(2005).
Heat transfer prediction of rotating rectangular channels using Reynolds stress model. Journal of Thermophysics and Heat Transfer.
19(1), 36-47.
-
Su, G. G., Chen, H. C., Han, J. C., & Heidmann, J. D.
(2004).
Computation of flow and heat transfer in rotating two-pass rectangular channels (AR=1 : 1, 1 : 2, and 1 : 4) with smooth walls by a Reynolds stress turbulence model. International Journal of Heat and Mass Transfer.
47(26), 5665-5683.
-
Kwak, J. S., Ahn, J. Y., & Han, J. C.
(2004).
Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade. International Journal of Heat and Mass Transfer.
47(26), 5651-5663.
-
Su, G. G., Teng, S. Y., Chen, H. C., & Han, J. C.
(2004).
Flow and heat-transfer computations in rotating rectangular channels with V-shaped ribs. Journal of Thermophysics and Heat Transfer.
18(4), 534-547.
-
Wright, L. M., Fu, W. L., & Han, J. C.
(2004).
Thermal performance of angled, V-shaped, and W-shaped rib turbulators in rotating rectangular cooling channels (AR=4:1). Journal of Turbomachinery.
126(4), 604-614.
-
Choi, J., Teng, S. Y., Han, J. C., & Ladeinde, F.
(2004).
Effect of free-stream turbulence on turbine blade heat transfer and pressure coefficients in low Reynolds number flows. International Journal of Heat and Mass Transfer.
47(14-16), 3441-3452.
-
Wright, L. M., Lee, E., & Han, J. C.
(2004).
Effect of rotation on heat transfer in rectangular channels with pin fins. Journal of Thermophysics and Heat Transfer.
18(2), 263-272.
-
Han, J.
(2004).
Recent Studies in Turbine Blade Cooling. International Journal of Rotating Machinery.
10(6), 443-457.
-
Lau, S. C., Cervantes, J., Han, J. C., Rudolph, R. J., & Flannery, K.
(2003).
Measurements of wall heat (mass) transfer for flow through blockages with round and square holes in a wide rectangular channel. International Journal of Heat and Mass Transfer.
46(21), 3991-4001.
-
Kwak, J. S., & Han, J. C.
(2003).
Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade. 125(4), 669-677.
-
Griffith, T. S., Al-Hadhrami, L., & Han, J. C.
(2003).
Heat transfer in rotating rectangular cooling channels (AR = 4) with dimples. Journal of Turbomachinery.
125(3), 555-563.
-
Kwak, J. S., & Han, J. C.
(2003).
Heat transfer coefficients and film-cooling effectiveness on a gas turbine blade tip. 125(3), 494-502.
-
Al-Hadhrami, L., Griffith, T., & Han, J. C.
(2003).
Heat transfer in two-pass rotating rectangular channels (AR=2) with five different orientations of 45 deg V-shaped rib turbulators. 125(2), 232-242.
-
Al-Qahtani, M., Chen, H. C., & Han, J. C.
(2003).
A numerical study of flow and heat transfer in rotating rectangular channels (AR=4) with 45 deg rib turbulators by Reynolds stress turbulence model. Journal of Heat Transfer.
125(1), 19-26.
-
Al-Hadhrami, L., & Han, J. C.
(2003).
Effect of rotation on heat transfer in two-pass square channels with five different orientations of 45 degrees angled rib turbulators. International Journal of Heat and Mass Transfer.
46(4), 653-669.
-
Chandra, P. R., Alexander, C. R., & Han, J. C.
(2003).
Heat transfer and friction behaviors in rectangular channels with varying number of ribbed walls. 46(3), 481-495.
-
Kwak, J. S., & Han, J. C.
(2003).
Heat-transfer coefficients of a turbine blade-tip and near-tip regions. Journal of Thermophysics and Heat Transfer.
17(3), 297-303.
-
Son, S. Y., Kihm, K. D., & Han, J. C.
(2002).
PIV flow measurements for heat transfer characterization in two-pass square channels with smooth and 90 degrees ribbed walls. 45(24), 4809-4822.
-
Griffith, T. S., Al-Hadhrami, L., & Han, J. C.
(2002).
Heat transfer in rotating rectangular cooling channels (AR=4) with angled ribs. Journal of Heat Transfer.
124(4), 617-625.
-
Azad, G. S., Han, J. C., Bunker, R. S., & Lee, C. P.
(2002).
Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer. 124(3), 452-459.
-
AZAD, G. M., HUANG, Y., & HAN, J.
(2002).
Jet Impingement Heat Transfer on Pinned Surfaces Using a Transient Liquid Crystal Technique. International Journal of Rotating Machinery.
8(3), 161-173.
-
Al-Qahtani, M., Jang, Y. J., Chen, H. C., & Han, J. C.
(2002).
Flow and heat transfer in rotating two-pass rectangular channels (AR=2) by Reynolds stress turbulence model. 45(9), 1823-1838.
-
Teng, S., Han, J. C., & Azad, G.
(2001).
Detailed heat transfer coefficient distributions on a large-scale gas turbine blade tip. 123(4), 803-809.
-
Teng, S., Han, J. C., & Poinsatte, P. E.
(2001).
Effect of film-hole shape on turbine-blade film-cooling performance. Journal of Thermophysics and Heat Transfer.
15(3), 257-265.
-
Jang, Y. J., Chen, H. C., & Han, J. C.
(2001).
Computation of flow and heat transfer in two-pass channels with 60 deg ribs. Journal of Heat Transfer.
123(3), 563-575.
-
Du, H., Ekkad, S. V., Han, J., & Lee, C. P.
(2001).
Detailed Film Cooling Measurements over a Gas Turbine Blade Using a Transient Liquid Crystal Image Technique. International Journal of Rotating Machinery.
7(6), 415-424.
-
Teng, S., Han, J. C., & Poinsatte, P. E.
(2001).
Effect of Film-Hole Shape on Turbine-Blade Heat-Transfer Coefficient Distribution. Journal of Thermophysics and Heat Transfer.
15(3), 249-256.
-
Jang, Y., Chen, H., & Han, J.
(2001).
Numerical Prediction of Flow and Heat Transfer in a Two-pass Square Channel with 90 Ribs. International Journal of Rotating Machinery.
7(3), 195-208.
-
Parsons, J. A., & Han, J.
(2001).
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels with Film Coolant Extraction. International Journal of Rotating Machinery.
7(2), 87-103.
-
Ekkad, S. V., & Han, J. C.
(2000).
A transient liquid crystal thermography technique for gas turbine heat transfer measurements. 11(7), 957-968.
-
Chen, H. C., Jang, Y. J., & Han, J. C.
(2000).
Computation of heat transfer in rotating two-pass square channels by a second-moment closure model. International Journal of Heat and Mass Transfer.
43(9), 1603-1616.
-
Ekkad, S. V., & Han, J. C.
(2000).
Film cooling measurements on cylindrical models with simulated thermal barrier coating spallation. Journal of Thermophysics and Heat Transfer.
14(2), 194-200.
-
Ekkad, S., Huang, Y. Z., & Han, J. C.
(2000).
Impingement heat transfer measurements under an array of inclined jets. Journal of Thermophysics and Heat Transfer.
14(2), 286-288.
-
Azad, G. S., Huang, Y. H., & Han, J. C.
(2000).
Impingement heat transfer on dimpled surfaces using a transient liquid crystal technique. Journal of Thermophysics and Heat Transfer.
14(2), 186-193.
-
Zhang, Y. M., Azad, G. M., Han, J. C., & Lee, C. P.
(2000).
Turbulent Heat Transfer Enhancement and Surface Heating Effect in Square Channels with Wavy, and Twisted Tape Inserts with Interrupted Ribs. Journal of Enhanced Heat Transfer.
7(1), 35-49.
-
Ekkad, S. V., Huang, Y. Z., & Han, J. C.
(1999).
Impingement heat transfer on a target plate with film cooling holes. Journal of Thermophysics and Heat Transfer.
13(4), 522-528.
-
Du, H., Ekkad, S. V., & Han, J. C.
(1999).
Effect of unsteady wake with trailing edge coolant ejection on film cooling performance for a gas turbine blade. Journal of Turbomachinery.
121(3), 448-455.
-
Akella, K. V., & Han, J. C.
(1999).
Impingement cooling in rotating two-pass rectangular channels with ribbed walls. Journal of Thermophysics and Heat Transfer.
13(3), 364-371.
-
Ekkad, S. V., & Han, J. C.
(1999).
Heat transfer distributions on a cylinder with simulated thermal barrier coating spallation. Journal of Thermophysics and Heat Transfer.
13(1), 76-81.
-
Ekkad, S. V., Krishna, A., & Han, J. C.
(1998).
Detailed film cooling measurements on a cylindrical model with simulated TBC spallation. ASME -Publications- Htd.
357(4), 69-76.
-
Ekkad, S. V., Huang, Y. Z., & Han, J. C.
(1998).
Detailed heat transfer distributions in two-pass square channels with rib turbulators and bleed holes. 41(23), 3781-3791.
-
Ekkad, S. V., Han, J. C., & Du, H.
(1998).
Detailed film cooling measurements on a cylindrical leading edge model: Effect of free-stream turbulence and coolant density. Journal of Turbomachinery.
120(4), 799-807.
-
Du, H., Han, J. C., & Ekkad, S. V.
(1998).
Effect of unsteady wake on detailed heat transfer coefficient and film effectiveness distributions for a gas turbine blade. Journal of Turbomachinery.
120(4), 808-817.
-
Parsons, J. A., & Han, J. C.
(1998).
Rotation effect on jet impingement heat transfer in smooth rectangular channels with heated target walls and radially outward cross flow. 41(13), 2059-2071.
-
Huang, Y. Z., Ekkad, S. V., & Han, J. C.
(1998).
Detailed heat transfer distributions under an array of orthogonal impinging jets. Journal of Thermophysics and Heat Transfer.
12(1), 73-79.
-
Mehendale, A. B., Jiang, H. W., Ekkad, S. V., & Han, J.
(1998).
Effect of Film Injection Location on Local Heat Transfer Coefficient on a Gas Turbine Blade. International Journal of Rotating Machinery.
4(3), 163-174.
-
Parsons, J. A., Han, J. C., & Lee, C. P.
(1998).
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Radially Outward Crossflow. Journal of Turbomachinery.
120(1), 79-85.
-
Kim, S. Y., & Han, J.
(1998).
Surface Heating Effect on Local Heat Transfer in an Inclosed Corotating Disks with Axial Throughflow. International Journal of Fluid Mechanics Research.
25(4-6), 742-752.
-
Ekkad, S. V., Mehendale, A. B., Han, J. C., & Lee, C. P.
(1997).
Combined effect of grid turbulence and unsteady wake on film effectiveness and heat transfer coefficient of a gas turbine blade with air and CO2 film injection. Journal of Turbomachinery.
119(3), 594-600.
-
Ekkad, S. V., & Han, J. C.
(1997).
Detailed heat transfer distributions in two-pass square channels with rib turbulators. 40(11), 2525-2537.
-
Ekkad, S. V., Zapata, D., & Han, J. C.
(1997).
Film effectiveness over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method. Journal of Turbomachinery.
119(3), 587-593.
-
Du, H., Ekkad, S., & Han, J. C.
(1997).
Effect of unsteady wake with trailing edge coolant ejection on detailed heat transfer coefficient distributions for a gas turbine blade. Journal of Heat Transfer.
119(2), 242-248.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1997).
Turbulent flow and heat transfer in rotating different aspect ratio channels. Journal of Thermophysics and Heat Transfer.
11(2), 318-319.
-
Zhang, Y. M., Han, J. C., & Lee, C. P.
(1997).
Heat Transfer and Friction Characteristics of Turbulent Flow in Circular Tubes with Twisted-Tape Inserts and Axial Interrupted Ribs. Journal of Enhanced Heat Transfer.
4(4), 297-308.
-
Huang, Y., Ekkad, S. V., & Han, J. C.
(1996).
Detailed heat transfer coefficient distributions under an array of impinging jets with coolant extraction. ASME -Publications- Htd.
333, 143-150.
-
Ekkad, S. V., Huang, Y., & Han, J. C.
(1996).
Detailed heat transfer distributions in two-pass smooth and turbulated square channels with bleed holes. ASME -Publications- Htd.
330, 133-140.
-
Ekkad, S. V., Han, J., & Du, H.
(1996).
SURFACE HEAT TRANSFER VISUALIZATION ON A MODEL GAS TURBINE BLADE USING A TRANSIENT LIQUID CRYSTAL IMAGE TECHNIQUE. Journal of Flow Visualization and Image Processing.
3(2-3), 141-152.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1996).
On flow separation with adverse rotational buoyancy. Journal of Heat Transfer.
118(4), 977-979.
-
Dutta, S., & Han, J. C.
(1996).
Local heat transfer in rotating smooth and ribbed two-pass square channels with three channel orientations. Journal of Heat Transfer.
118(3), 578-584.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1996).
Prediction of turbulent heat transfer in rotating smooth square ducts. International Journal of Heat and Mass Transfer.
39(12), 2505-2514.
-
Ekkad, S. V., & Han, J. C.
(1996).
Heat transfer inside and downstream of cavities using transient liquid crystal method. Journal of Thermophysics and Heat Transfer.
10(3), 511-516.
-
Dutta, S., Han, J. C., Zhang, Y., & Lee, C. P.
(1996).
Local heat transfer in a rotating two-pass triangular duct with smooth walls. Journal of Turbomachinery.
118(3), 435-443.
-
Jiang, H. W., & Han, J. C.
(1996).
Effect of film hole row location on film effectiveness on a gas turbine blade. Journal of Heat Transfer.
118(2), 327-333.
-
Dutta, S., Han, J. C., & Lee, C. P.
(1996).
Local heat transfer in a rotating two-pass ribbed triangular duct with two model orientations. International Journal of Heat and Mass Transfer.
39(4), 707-715.
-
Ekkad, S. V., Du, H., & Han, J.
(1996).
LOCAL HEAT TRANSFER COEFFICIENT AND FILM EFFECTIVENESS DISTRIBUTIONS ON A CYLINDRICAL LEADING EDGE MODEL USING A TRANSIENT LIQUID CRYSTAL IMAGE METHOD. Journal of Flow Visualization and Image Processing.
3(2-3), 129-140.
-
Dutta, S., Han, J. C., & Lee, C. P.
(1995).
Experimental heat transfer in a rotating triangular duct: Effect of model orientation. Journal of Heat Transfer.
117(4), 1058-1061.
-
ZHANG, L., & HAN, J. C.
(1995).
COMBINED EFFECT OF FREE-STREAM TURBULENCE AND UNSTEADY WAKE ON HEAT-TRANSFER COEFFICIENTS FROM A GAS-TURBINE BLADE. Journal of Heat Transfer.
117(2), 296-302.
-
PARSONS, J. A., HAN, J. C., & ZHANG, Y. M.
(1995).
Effect of model orientation and wall heating condition on local heat transfer in a rotating two-pass square channel with rib turbulators. 38(7), 1151-1159.
-
DUTTA, S., ANDREWS, M. J., & HAN, J. C.
(1995).
SIMULATION OF TURBULENT HEAT-TRANSFER IN A ROTATING DUCT. Journal of Thermophysics and Heat Transfer.
9(2), 381-382.
-
ZHANG, Y. M., HAN, J. C., PARSONS, J. A., & LEE, C. P.
(1995).
SURFACE HEATING EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH 60-DEG ANGLED RIB TURBULATORS. Journal of Turbomachinery.
117(2), 272-280.
-
Dutta, S., Han, J., & Zhang, Y.
(1995).
Influence of Rotation on Heat Transfer from a Two-Pass Channel with Periodically Placed Turbulence and Secondary Flow Promoters. International Journal of Rotating Machinery.
1(2), 129-144.
-
Dutta, S., Han, J. C., & Lee, C. P.
(1994).
Effect of model orientation on local heat transfer in a rotating two-pass smooth triangular duct. ASME -Publications- Htd.
300, 147-153.
-
ZHANG, L., & HAN, J. C.
(1994).
INFLUENCE OF MAINSTREAM TURBULENCE ON HEAT-TRANSFER COEFFICIENTS FROM A GAS-TURBINE BLADE. Journal of Heat Transfer.
116(4), 896-903.
-
MEHENDALE, A. B., EKKAD, S. V., & HAN, J. C.
(1994).
MAINSTREAM TURBULENCE EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER COEFFICIENT OF A GAS-TURBINE BLADE WITH AIR AND CO2 FILM INJECTION. International Journal of Heat and Mass Transfer.
37(17), 2707-2714.
-
OU, S., & HAN, J. C.
(1994).
UNSTEADY WAKE EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER COEFFICIENT FROM A TURBINE BLADE WITH ONE ROW OF AIR AND CO2 FILM INJECTION. Journal of Heat Transfer.
116(4), 921-928.
-
MEHENDALE, A. B., HAN, J. C., OU, S., & LEE, C. P.
(1994).
UNSTEADY WAKE OVER A LINEAR TURBINE BLADE CASCADE WITH AIR AND CO2 FILM INJECTION .2. EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER DISTRIBUTIONS. Journal of Turbomachinery.
116(4), 730-737.
-
OU, S. C., & HAN, J. C.
(1994).
LEADING-EDGE FILM-COOLING HEAT-TRANSFER THROUGH ONE ROW OF INCLINED FILM SLOTS AND HOLES INCLUDING MAINSTREAM TURBULENCE EFFECTS. Journal of Heat Transfer.
116(3), 561-569.
-
ZHANG, Y. M., GU, W. Z., & HAN, J. C.
(1994).
AUGMENTED HEAT-TRANSFER IN TRIANGULAR DUCTS WITH FULL AND PARTIAL RIBBED WALLS. Journal of Thermophysics and Heat Transfer.
8(3), 574-579.
-
PARSONS, J. A., HAN, J. C., & ZHANG, Y. M.
(1994).
WALL HEATING EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH 90-DEGREES RIB TURBULATORS. International Journal of Heat and Mass Transfer.
37(9), 1411-1420.
-
ZHANG, Y. M., GU, W. Z., & HAN, J. C.
(1994).
HEAT-TRANSFER AND FRICTION IN RECTANGULAR CHANNELS WITH RIBBED OR RIBBED-GROOVED WALLS. Journal of Heat Transfer.
116(1), 58-65.
-
KIM, S. Y., HAN, J. C., MORRISON, G. L., & ELOVIC, E.
(1994).
LOCAL HEAT-TRANSFER IN ENCLOSED CO-ROTATING DISKS WITH AXIAL THROUGHFLOW. Journal of Heat Transfer.
116(1), 66-72.
-
Zhang, Y. M., Gu, W., & Han, J. C.
(1994).
Heat Transfer and Friction in Triangular Ducts with Turbulence Promoters. 8(3), 574-579.
-
HAN, J. C., ZHANG, Y. M., & LEE, C. P.
(1994).
INFLUENCE OF SURFACE HEATING CONDITION ON LOCAL HEAT-TRANSFER IN A ROTATING SQUARE CHANNEL WITH SMOOTH WALLS AND RADIAL OUTWARD FLOW. Journal of Turbomachinery.
116(1), 149-158.
-
HAN, J. C., ZHANG, L., & OU, S.
(1993).
INFLUENCE OF UNSTEADY WAKE ON HEAT-TRANSFER COEFFICIENT FROM A GAS-TURBINE BLADE. Journal of Heat Transfer.
115(4), 904-911.
-
HAN, J. C., ZHANG, Y. M., & KALKUEHLER, K.
(1993).
UNEVEN WALL TEMPERATURE EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH SMOOTH WALLS. Journal of Heat Transfer.
115(4), 912-920.
-
Mehendale, A. B., & Han, J.
(1993).
Reynolds number effect on leading edge film effectiveness and heat transfer coefficient. International Journal of Heat and Mass Transfer.
36(15), 3723-3730.
-
Han, J., Huang, J. J., & Lee, C.
(1993).
Augmented Heat Transfer in Square Channels with Wedge-Shaped and Delta-Shaped Turbulence Promoters. 1(1), 37-52.
-
HAN, J. C., & ZHANG, Y. M.
(1992).
EFFECT OF UNEVEN WALL TEMPERATURE ON LOCAL HEAT-TRANSFER IN A ROTATING SQUARE CHANNEL WITH SMOOTH WALLS AND RADIAL OUTWARD FLOW. Journal of Heat Transfer.
114(4), 850-858.
-
PARK, J. S., HAN, J. C., HUANG, Y., OU, S., & BOYLE, R. J.
(1992).
Heat transfer performance comparisons of five different rectangular channels with parallel angled ribs. 35(11), 2891-2903.
-
MEHENDALE, A. B., & HAN, J. C.
(1992).
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE FILM COOLING HEAT-TRANSFER. Journal of Turbomachinery.
114(4), 707-715.
-
Ou, S., Mehendale, A. B., & Han, J. C.
(1992).
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location. Journal of Turbomachinery.
114(4), 716-723.
-
Ou, S., & Han, J. C.
(1992).
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots. Journal of Turbomachinery.
114(4), 724-733.
-
HAN, J. C., & ZHANG, Y. M.
(1992).
HIGH-PERFORMANCE HEAT-TRANSFER DUCTS WITH PARALLEL BROKEN AND V-SHAPED BROKEN RIBS. International Journal of Heat and Mass Transfer.
35(2), 513-523.
-
YOUNG, C. D., HAN, J. C., HUANG, Y., & RIVIR, R. B.
(1992).
INFLUENCE OF JET-GRID TURBULENCE ON FLAT-PLATE TURBULENT BOUNDARY-LAYER FLOW AND HEAT-TRANSFER. Journal of Heat Transfer.
114(1), 65-72.
-
Mehendale, A. B., & Han, J. C.
(1992).
Influence of high mainstream turbulence on leading edge film cooling heat transfer: effect of film hole spacing. International Journal of Heat and Mass Transfer.
35(10), 2593-2604.
-
Han, J. C., Zhang, Y. M., & Lee, C. P.
(1992).
Influence of surface heat flux ratio on heat transfer augmentation in square channels with parallel, crossed, and V-shaped angled ribs. Journal of Turbomachinery.
114(4), 872-880.
-
MEHENDALE, A. B., HAN, J. C., & OU, S.
(1991).
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE HEAT-TRANSFER. Journal of Heat Transfer.
113(4), 843-850.
-
KUMARAN, T. K., HAN, J. C., & LAU, S. C.
(1991).
AUGMENTED HEAT-TRANSFER IN A PIN FIN CHANNEL WITH SHORT OR LONG EJECTION HOLES. International Journal of Heat and Mass Transfer.
34(10), 2617-2628.
-
HAN, J. C., ZHANG, Y. M., & LEE, C. P.
(1991).
AUGMENTED HEAT-TRANSFER IN SQUARE CHANNELS WITH PARALLEL, CROSSED, AND V-SHAPED ANGLED RIBS. Journal of Heat Transfer.
113(3), 590-596.
-
LAU, S. C., MCMILLIN, R. D., & HAN, J. C.
(1991).
TURBULENT HEAT-TRANSFER AND FRICTION IN A SQUARE CHANNEL WITH DISCRETE RIB TURBULATORS. Journal of Turbomachinery.
113(3), 360-366.
-
Parken, W. H., Fletcher, L. S., Sernas, V., & Han, J. C.
(1990).
Heat Transfer Through Falling Film Evaporation and Boiling on Horizontal Tubes. Journal of Heat Transfer.
112(3), 744-750.
-
Han, J. C., & Zhang, P.
(1989).
Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators. Journal of Turbomachinery.
111(4), 515-521.
-
HAN, J. C., OU, S., PARK, J. S., & LEI, C. K.
(1989).
AUGMENTED HEAT-TRANSFER IN RECTANGULAR CHANNELS OF NARROW ASPECT RATIOS WITH RIB TURBULATORS. International Journal of Heat and Mass Transfer.
32(9), 1619-1630.
-
Lau, S. C., Ong, L. E., & Han, J. C.
(1989).
Conjugate heat transfer in channels with internal longitudinal fins. Journal of Thermophysics and Heat Transfer.
3(3), 303-308.
-
Chandra, P. R., & Han, J. C.
(1989).
Pressure drop and mass transfer in two-pass ribbed channels. Journal of Thermophysics and Heat Transfer.
3(3), 315-320.
-
Lau, S. C., Han, J. C., & Batten, T.
(1989).
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes. Journal of Turbomachinery.
111(2), 116-123.
-
LAU, S. C., HAN, J. C., & KIM, Y. S.
(1989).
TURBULENT HEAT-TRANSFER AND FRICTION IN PIN FIN CHANNELS WITH LATERAL FLOW EJECTION. Journal of Heat Transfer.
111(1), 51-58.
-
HAN, J. C.
(1988).
HEAT-TRANSFER AND FRICTION CHARACTERISTICS IN RECTANGULAR CHANNELS WITH RIB TURBULATORS. Journal of Heat Transfer.
110(2), 321-328.
-
Chandra, P. R., Han, J. C., & Lau, S. C.
(1988).
Effect of Rib Angle on Local Heat/Mass Transfer Distribution in a Two-Pass Rib-Roughened Channel. Journal of Turbomachinery.
110(2), 233-241.
-
Han, J. C., Chandra, P. R., & Lau, S. C.
(1988).
Local Heat/Mass Transfer Distributions Around Sharp 180 deg Turns in Two-Pass Smooth and Rib-Roughened Channels. Journal of Heat Transfer.
110(1), 91-98.
-
CHANDRA, P. R., HAN, J. C., & LAU, S. C.
(1988).
EFFECT OF RIB ANGLE ON LOCAL HEAT MASS-TRANSFER DISTRIBUTION IN A 2-PASS RIB-ROUGHENED CHANNEL. Journal of Turbomachinery.
110(2), 233-241.
-
HAN, J. C., & PARK, J. S.
(1988).
DEVELOPING HEAT-TRANSFER IN RECTANGULAR CHANNELS WITH RIB TURBULATORS. International Journal of Heat and Mass Transfer.
31(1), 183-195.
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1987).
Local endwall heat/mass-transfer distributions in pin fin channels. Journal of Thermophysics and Heat Transfer.
1(4), 365-372.
-
HAN, J. C., & MEHENDALE, A. B.
(1986).
FLAT-PLATE FILM COOLING WITH STEAM INJECTION THROUGH ONE ROW AND 2 ROWS OF INCLINED HOLES. Journal of Turbomachinery.
108(1), 137-144.
-
HAN, J. C., & FLETCHER, L. S.
(1985).
FALLING FILM EVAPORATION AND BOILING IN CIRCUMFERENTIAL AND AXIAL GROOVES ON HORIZONTAL TUBES. Industrial and Engineering Chemistry Process Design and Development.
24(3), 570-575.
-
Han, J. C., Park, J. S., & Lei, C. K.
(1985).
Heat Transfer Enhancement in Channels With Turbulence Promoters. Journal of Engineering for Gas Turbines and Power.
107(3), 628-635.
-
HAN, J. C.
(1984).
HEAT-TRANSFER AND FRICTION IN CHANNELS WITH 2 OPPOSITE RIB-ROUGHENED WALLS. Journal of Heat Transfer.
106(4), 774-781.
-
HAN, J. C., & YANG, W. J.
(1981).
TRANSIENT NUCLEATION AND BUBBLE-GROWTH IN IMMISCIBLE LIQUID COMPOSITES INDUCED BY COUNTERDIFFUSION OF GASES. Letters in Heat and Mass Transfer.
8(1), 11-24.
-
Han, J., & Yang, W.
(1980).
Thermal instability in spherical liquid shells induced by surface tension. Letters in Heat and Mass Transfer.
7(5), 363-378.
-
Han, J. C., & Yang, W.
(1980).
Thermal Instability in Liquid Droplets on a Heated Surface. Journal of Heat Transfer.
102(3), 581-583.
-
Han, J. C., French, C. L., & Hendry, J. W.
(1980).
The New Thermal Cycling Process for Structural Foam Smooth Surface. 10-14.
-
Han, J. C., French, C. L., & Hendry, J. W.
(1979).
Structural Foam Surface Finishes are Practically Perfect Now. Modern Plastics.
44-45.
-
Han, J. C., Glicksman, L. R., & Rohsenow, W. M.
(1978).
An investigation of heat transfer and friction for rib-roughened surfaces. International Journal of Heat and Mass Transfer.
21(8), 1143-1156.
-
Alsaleem, S. M., Wright, L. M., & Han, J.
(2021).
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations. Journal of Turbomachinery.
143(9),
-
book
-
Han, J., & Wright, L. M.
(2020).
Experimental Methods in Heat Transfer and Fluid Mechanics. CRC Press.
-
Han, J., Dutta, S., & Ekkad, S.
(2012).
Gas Turbine Heat Transfer and Cooling Technology, Second Edition. CRC Press.
-
Han, J. C., Dutta, S., & Ekkad, S.
(2012).
Gas Turbine Heat Transfer and Cooling Technology
-
Han, J.
(2011).
Analytical Heat Transfer. CRC Press.
-
Han, J., Dutta, S., & Ekkad, S. V.
(2004).
Gas Turbine Heat Transfer and Cooling Technology
-
Han, J., & Wright, L. M.
(2020).
Experimental Methods in Heat Transfer and Fluid Mechanics. CRC Press.
-
chapter
-
Han, J. C., Ekkad, S. V., & Huang, Y.
(1996).
Measurements on Augmented Heat Transfer Surfaces Using a Transient Liquid Crystal Technique. Bergles, A. E., Kraus, A. D., & Manglik, R. M. (Eds.),
Process, Enhanced, and Multiphase Heat Transfer A Festschrift for A.E. Bergles.
(pp. 339-349).
Begel House.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1994).
Heat Transfer and Flow Predictions in a Rotating Square Duct with Coriolis-Modified Turbulence Models. Heat Transfer 1994.
(pp. 219-224).
IChemE.
-
Kim, S. Y., & Han, J. C.
(1993).
Surface Heating Effect on Local Heat Transfer in an Enclosed CoRotating Disks with Axial Throughflow. Transport Phenomena in Thermal Engineering.
(pp. 1296-1301).
-
Zhang, Y. M., Gu, W., & Han, J. C.
(1992).
Heat Transfer in a Five-Pass Irregular Channel With and Without Pin Fins. Kim, J. H., & Yang, W. J. (Eds.),
Rotating Machinery 3rd International Symposium on Transport Phenomena and Dynamics of Rotating Machinery : Papers.
(pp. 121-128).
Hemisphere Publishing Company.
-
Lau, S. C., Han, J. C., & Batten, T.
(1989).
Heat Transfer and Friction in Cooling Channels Near Trailing Edges of Turbine Blades. Yang, W. J., & Kim, J. H. (Eds.),
Transport Phenomena.
(pp. 391-410).
CRC Press.
-
Han, J. C.
(1989).
Augmented Heat Transfer in Turbine Cooling Passages. Hwang, G. J. (Eds.),
Transport Phenomena In Thermal Control Cooling Technologies for Electronic Equipment & Rotating Machinery.
(pp. 311-330).
CRC Press.
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1987).
Local Heat Transfer in Channels with Pin Fins Via the Naphthalene Sublimation Technique. Yang, W. J. (Eds.),
Heat Transfer and Fluid Flow in Rotating Machinery.
(pp. 64-75).
Hemisphere Pub.
-
Han, J. C., & Yang, W. J.
(1982).
Visualization of Flow Patterns in Plastic Injection Molds. Merzkirch, W. (Eds.),
Flow Visualization II Proceedings of the Second International Symposium on Flow Visualization, September 9-12, 1980, Bochum, West Germany.
(pp. 579-583).
Taylor & Francis Group.
-
Han, J. C., Ekkad, S. V., & Huang, Y.
(1996).
Measurements on Augmented Heat Transfer Surfaces Using a Transient Liquid Crystal Technique. Bergles, A. E., Kraus, A. D., & Manglik, R. M. (Eds.),
Process, Enhanced, and Multiphase Heat Transfer A Festschrift for A.E. Bergles.
(pp. 339-349).
Begel House.
-
conference paper
-
Chowdhury, N., Shiau, C., Han, J., Xu, H., & Fox, M.
(2018).
FILM COOLING EFFECTIVENESS COMPARISON ON TURBINE VANE ENDWALL WITH CLUSTER CONFIGURATIONS USING PSP MEASUREMENT TECHNIQUE. v008t10a039-v008t10a039.
-
Shiau, C., Chen, A. F., Han, J., Azad, S., & Lee, C.
(2017).
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using PSP Technique. v05ct19a028-v05ct19a028.
-
Zhang, M., Wang, N., Chen, A. F., & Han, J.
(2017).
Influence of Turbine Blade Leading Edge Profile on Film Cooling With Shaped Holes. v05ct19a010-v05ct19a010.
-
Wang, N., Chen, A. F., Zhang, M., & Han, J.
(2017).
TURBINE BLADE LEADING EDGE COOLING WITH ONE ROW OF NORMAL OR TANGENTIAL IMPINGING JETS. v05at16a007-v05at16a007.
-
Shiau, C., Chowdhury, N., Han, J., Mirzamoghadam, A. V., & Riahi, A.
(2017).
Transonic Turbine Vane Suction Side Film Cooling With Showerhead Effect Using PSP Measurement Technique. v05ct19a002-v05ct19a002.
-
Chen, A. F., Shiau, C., & Han, J.
(2017).
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions. v05ct19a001-v05ct19a001.
-
Chowdhury, N., Shiau, C., Han, J., Zhang, L., & Moon, H.
(2017).
Turbine Vane Endwall Film Cooling From Cross-Row Configuration With Simulated Upstream Leakage Flow. v05ct19a004-v05ct19a004.
-
Chowdhury, N., Shiau, C., Han, J., Zhang, L., & Moon, H.
(2017).
Turbine Vane Endwall Film Cooling Study From Axial-Row Configuration With Simulated Upstream Leakage Flow. v05ct19a003-v05ct19a003.
-
Shiau, C., Chowdhury, N., Yang, S., Han, J., MirzaMoghadam, A., & Riahi, A.
(2016).
HEAT TRANSFER COEFFICIENTS AND FILM COOLING EFFECTIVENESS OF TRANSONIC TURBINE VANE SUCTION SURFACE USING TSP TECHNIQUE. v05ct19a010-v05ct19a010.
-
Chen, A. F., Shiau, C., & Han, J.
(2016).
TURBINE BLADE PLATFORM FILM COOLING WITH SIMULATED SWIRL PURGE FLOW AND SLASHFACE LEAKAGE CONDITIONS. v05ct19a012-v05ct19a012.
-
Chowdhury, N., Shiau, C., Han, J., Zhang, L., & Moon, H.
(2016).
TURBINE VANE ENDWALL FILM COOLING WITH SLASHFACE LEAKAGE AND DISCRETE HOLE CONFIGURATION. v05ct19a011-v05ct19a011.
-
Chowdhury, N., Zirakzadeh, H., & Han, J.
(2015).
A PREDICTIVE MODEL FOR PRELIMINARY GAS TURBINE BLADE COOLING ANALYSIS. v05bt13a002-v05bt13a002.
-
Shiau, C., Chen, A. F., Han, J., Azad, S., & Lee, C.
(2015).
FULL-SCALE TURBINE VANE END-WALL FILM-COOLING EFFECTIVENESS DISTRIBUTION USING PSP TECHNIQUE. v05bt12a007-v05bt12a007.
-
Yang, S., Han, J., MirzaMoghadam, A., & Riahi, A.
(2015).
Film Cooling Effectiveness of Transonic Turbine Vane Suction Side with Compound-Angle shaped hole configuration. v05bt12a005-v05bt12a005.
-
Li, S., Yang, S., Han, J., Zhang, L., & Moon, H.
(2015).
TURBINE BLADE SURFACE PHANTOM COOLING FROM UPSTREAM NOZZLE TRAILING EDGE EJECTION. v05bt12a003-v05bt12a003.
-
Li, S., Lee, J., Han, J., Zhang, L., & Moon, H.
(2015).
TURBINE PLATFORM COOLING AND BLADE SUCTION SURFACE PHANTOM COOLING FROM SIMULATED SWIRL PURGE FLOW. v05bt12a011-v05bt12a011.
-
Wu, H., Zirakzadeh, H., Han, J., Zhang, L., & Moon, H.
(2015).
HEAT TRANSFER IN A RIB AND PIN ROUGHENED ROTATING MULTI-PASS CHANNEL WITH HUB TURNING VANE AND TRAILING-EDGE SLOT EJECTION. v05at11a007-v05at11a007.
-
Ekkad, S., & Han, J.
(2014).
A REVIEW OF HOLE GEOMETRY AND COOLANT DENSITY EFFECT ON FILM COOLING. v003t20a003-v003t20a003.
-
Wright, L. M., & Han, J.
(2014).
HEAT TRANSFER ENHANCEMENT FOR TURBINE BLADE INTERNAL COOLING. v003t23a005-v003t23a005.
-
Chen, A. F., Li, S., & Han, J.
(2014).
FILM COOLING WITH FORWARD AND BACKWARD INJECTION FOR CYLINDRICAL AND FAN-SHAPED HOLES USING PSP MEASUREMENT TECHNIQUE. v05bt13a042-v05bt13a042.
-
Rezasoltani, M., Lu, K., Schobeiri, M. T., & Han, J. C.
(2014).
A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness under Rotation Condition. v05bt13a019-v05bt13a019.
-
Lu, K., Rezasoltani, M., Schobeiri, M. T., & Han, J. C.
(2014).
A Combined Numerical and Experimental Study of the Effect of Non-Axisymmetric Contouring on Performance and Film Cooling Behavior of a Rotating Turbine Endwall. v05bt13a020-v05bt13a020.
-
Narzary, D., Liu, K., Han, J., Mhetras, S., & Landis, K.
(2014).
TURBINE BLADE TIP FILM-COOLING AND HEAT TRANSFER MEASUREMENTS AT HIGH BLOWING RATIOS. v05bt13a025-v05bt13a025.
-
Li, S., Chen, A. F., Wang, W., & Han, J.
(2014).
Experimental and Computational Film Cooling with Backward Injection for Cylindrical and Fan-Shaped Holes. 3455-3469.
-
Li, S., Yang, S., & Han, J.
(2013).
EFFECT OF COOLANT DENSITY ON LEADING EDGE SHOWERHEAD FILM COOLING USING PSP MEASUREMENT TECHNIQUE. v03bt13a005-v03bt13a005.
-
Rezasoltani, M., Schobeiri, M. T., & Han, J. C.
(2013).
Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring. v03bt13a033-v03bt13a033.
-
Mhetras, S., Han, J., & Huth, M.
(2013).
HEAT TRANSFER AND PRESSURE LOSS MEASUREMENTS IN A TURBULATED HIGH ASPECT RATIO CHANNEL WITH LARGE REYNOLDS NUMBER FLOWS. v03at12a051-v03at12a051.
-
Rallabandi, A., Lei, J., Han, J., Azad, S., & Lee, C.
(2013).
HEAT TRANSFER MEASUREMENTS IN ROTATING BLADE-SHAPE SERPENTINE COOLANT PASSAGE WITH RIBBED WALLS AT HIGH REYNOLDS NUMBERS. v03at12a004-v03at12a004.
-
Lei, J., Li, S., Han, J., Zhang, L., & Moon, H.
(2013).
Heat Transfer in Rotating Multi-Pass Rectangular Smooth Channel with and without a Turning Vane in Hub Region. 435-445.
-
Yang, S., Han, J., Azad, S., & Lee, C.
(2013).
Heat Transfer in Rotating Serpentine Coolant Passage with Ribbed Walls at Low Mach Numbers. v03at12a009-v03at12a009.
-
Mhetras, S., Han, J., & Huth, M.
(2013).
IMPINGEMENT HEAT TRANSFER FROM JET ARRAYS ON TURBULATED TARGET WALLS AT LARGE REYNOLDS NUMBERS. v03at12a052-v03at12a052.
-
Liu, K., Yang, S., & Han, J.
(2013).
INFLUENCE OF COOLANT DENSITY ON TURBINE PLATFORM FILM-COOLING WITH STATOR-ROTOR PURGE FLOW AND COMPOUND-ANGLE HOLES. v03bt13a004-v03bt13a004.
-
Teloxa, J., Sierra, F. Z., Carrillo, F., Narzary, D., Lei, J., & Han, J.
(2013).
MEASUREMENT AND MODELLING OF BLADE TIP COOLING IN GAS TURBINES. v03bt13a034-v03bt13a034.
-
Lu, K., Schobeiri, M. T., & Han, J. C.
(2013).
Numerical Simulation of Film Cooling on Rotating Blade Tips within a High-Pressure Turbine. v03bt13a032-v03bt13a032.
-
Chu, H., Chen, H., & Han, J.
(2013).
Numerical Simulation of Flow and Heat Transfer in Rotating Cooling Passage with Turning Vane in Hub Region. v03at12a010-v03at12a010.
-
Liu, K., Yang, S., & Han, J.
(2012).
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING WITH AXIAL SHAPED HOLES. 757-767.
-
Lei, J., Li, S., Han, J., Zhang, L., & Moon, H.
(2012).
HEAT TRANSFER IN ROTATING MULTI-PASS RECTANGULAR RIBBED CHANNEL WITH AND WITHOUT A TURNING VANE. 435-+.
-
Liu, K., Yang, S., & Han, J.
(2012).
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING WITH COMPOUND-ANGLE SHAPED HOLES. 1559-1569.
-
Schobeiri, M. T., Lu, K., & Han, J. C.
(2012).
Numerical Investigation of the Effect of Purge Flow on Aerodynamic Performance and Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring. 413-423.
-
Lei, J., Han, J., & Huh, M.
(2012).
EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO PASS RECTANGULAR CHANNEL (AR=2:1) AT HIGH ROTATION NUMBERS. 1329-1339.
-
Liu, K., Narzary, D. P., Han, J. C., Mirzamoghadam, A. V., & Riahi, A.
(2012).
INFLUENCE OF SHOCK WAVE ON TURBINE VANE SUCTION SIDE FILM COOLING WITH COMPOUND-ANGLE SHAPED HOLES. 447-457.
-
Li, S., Rallabandi, A. P., & Han, J.
(2011).
Influence of Unsteady Wake With Trailing Edge Coolant Ejection on Turbine Blade Film Cooling. 435-445.
-
Rallabandi, A. R., Liu, Y., & Han, J.
(2010).
HEAT TRANSFER IN TRAILING EDGE WEDGE-SHAPED PIN-FIN CHANNELS WITH SLOT EJECTION UNDER HIGH ROTATION NUMBERS. 369-380.
-
Huh, M., Lei, J., & Han, J.
(2010).
Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers. 53-65.
-
Narzary, D. P., Liu, K., Rallabandi, A. P., & Han, J.
(2010).
Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique. 1529-1540.
-
Rallabandi, A. P., Li, S., & Han, J.
(2010).
UNSTEADY WAKE AND COOLANT DENSITY EFFECTS ON TURBINE BLADE FILM COOLING USING PSP TECHNIQUE. 227-237.
-
Chang, B., Hung-Jue, S., Han, J., Wong, D., Kehr, A., Mallozzi, M., ... Snider, W.
(2009).
Residual stresses in 3LPO external pipeline coatings - Disbondment and cracking. 5-21.
-
Rallabandi, A. P., Grizzle, J., & Han, J.
(2009).
EFFECT OF UPSTREAM STEP ON FLAT PLATE FILM COOLING EFFECTIVENESS USING PSP. 599-609.
-
Rallabandi, A. P., Alkhamis, N., & Han, J.
(2009).
HEAT TRANSFER AND PRESSURE DROP MEASUREMENTS FOR A SQUARE CHANNEL WITH 45DEG ROUND EDGED RIBS AT HIGH REYNOLDS NUMBERS. 527-537.
-
Huh, M., Lei, J., Liu, Y., & Han, J.
(2009).
HIGH ROTATION NUMBER EFFECTS ON HEAT TRANSFER IN A RECTANGULAR (AR=2:1) TWO PASS CHANNEL. 383-394.
-
Sierra, F. Z., Narzary, D., Bolaina, C., Han, J. C., Kubiak, J., & Nebradt, J.
(2009).
Heat Transfer and Thermal Mechanical Stress Distributions in Gas Turbine Blades. 115-126.
-
Liu, Y., Huh, M., Han, J., & Moon, H.
(2009).
High Rotation Number Effect on Heat Transfer in a Triangular Channel With 45, Inverted 45, and 90 Ribs. 127-138.
-
Narzary, D. P., Liu, K., & Han, J.
(2009).
Influence of Coolant Density on Turbine Blade Platform Film-Cooling. 287-299.
-
Wright, L. M., Blake, S. A., & Han, J.
(2008).
Film cooling effectiveness distributions on a turbine blade cascade platform with stator-rotor purge and discrete film hole flows. Journal of Turbomachinery.
031015.
-
Lau, S. C., Cervantes, J., Han, J. C., & Rudolph, R. J.
(2008).
Internal cooling near trailing edge of a gas turbine airfoil with cooling airflow through blockages with holes. Journal of Turbomachinery.
031004.
-
Mhetras, S., Narzary, D., Gao, Z., & Han, J.
(2008).
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip. Journal of Turbomachinery.
021002-1413.
-
Huh, M., Liu, Y., Han, J., & Chopra, S.
(2008).
EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO-PASS RECTANGULAR CHANNEL (AR=1:4) WITH A SHARP ENTRANCE AT HIGH ROTATION NUMBERS. 287-300.
-
Mhetras, S., Han, J., & Rudolph, R.
(2008).
Film-Cooling Effectiveness From Shaped Film Cooling Holes for a Gas Turbine Blade. 837-848.
-
Liu, Y., Huh, M., Rhee, D., Han, J., & Moon, H.
(2008).
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels with Angled Ribs under High Rotation Numbers. 321-329.
-
Espinosa, F., Han, J. C., Portugal, A. U., Kubiak, J., Narzary, D., Blake, S., ... Nebradt, J.
(2008).
Influence of Cooling Flow Rate Variation on Gas Turbine Blade Temperature Distributions. 45-53.
-
Gao, Z., Narzary, D., & Han, J.
(2008).
Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling. 263-274.
-
Gao, Z., Narzary, D., Mhetras, S., & Han, J.
(2008).
Upstream vortex effects on turbine blade platform film cooling with typical stator-rotor purge flow. 707-718.
-
Gao, Z., Narzary, D. P., Mhetras, S., & Han, J.
(2008).
Full-coverage film cooling for a turbine blade with axial-shaped holes. Journal of Thermophysics and Heat Transfer.
50-61.
-
Liu, Y., Huh, M., Wright, L. M., & Han, J.
(2008).
Heat Transfer in Trailing Edge, Wedge Shaped Cooling Channels With Slot Ejection Under High Rotation Numbers. 311-320.
-
Wright, L. M., Blake, S., & Han, J.
(2007).
Effectiveness distributions on turbine-blade cascade platforms through simulated stator-rotor seals. Journal of Thermophysics and Heat Transfer.
754-762.
-
Gao, Z., Narzary, D., Mhetras, S., & Han, J.
(2007).
Full Coverage Film Cooling for a Turbine Blade with Axial Shaped Holes. 180-193.
-
Mhetras, S., Han, J., & Rudolph, R.
(2007).
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade. 93-103.
-
Gao, Z., Narzary, D., Mhetras, S., & Han, J.
(2007).
Effect of inlet flow angle on gas turbine blade tip film cooling. 43-53.
-
Narzary, D. P., Gao, Z., Mhetras, S., & Han, J.
(2007).
Effect of unsteady wake on film-cooling effectiveness distribution on a gas turbine blade with compound shaped holes. 79-91.
-
Suryanarayanan, A., Ozturk, B., Schobeiri, M. T., & Han, J. C.
(2007).
Film-cooling effectiveness on a rotating turbine platform using pressure sensitive paint technique. 169-183.
-
Gao, Z., Narzary, D. P., & Han, J.
(2007).
Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holes. 569-579.
-
Liu, Y., Huh, M., Han, J., & Chopra, S.
(2007).
Heat transfer in a two-pass rectangular channel (AR=1 : 4) under high rotation numbers. 55-65.
-
Yang, H., Gao, Z., Chen, H. C., Han, J. C., & Schobeiri, M. T.
(2007).
Prediction of film cooling and heat transfer on a rotating blade platform with stator-rotor purge and discrete film-hole flows in a 1-1/2 turbine stage. 67-77.
-
Wright, L. M., Blake, S. A., Rhee, D., & Han, J.
(2007).
Effect of upstream wake with vortex on turbine blade platform film cooling with simulated stator-rotor purge flow. 125-134.
-
Wright, L. M., Liu, Y., Han, J., & Chopra, S.
(2007).
Heat transfer in trailing edge, wedge-shaped cooling channels under high rotation numbers. 135-145.
-
Gao, Z., Yang, H., Wright, L., & Han, J. C.
(2006).
Conjugate prediction of leading edge film cooling and heat transfer. 181-189.
-
Mhetras, S., & Han, J.
(2006).
Effect of Unsteady Wake on Full Coverage Film-Cooling Effectiveness for A Gas Turbine Blade. 1382-1398.
-
Wright, L., Blake, S., & Han, J.
(2006).
Effectiveness Distributions on Turbine Blade Cascade Platforms through Simulated Stator-Rotor Seals. 1370-1381.
-
Fu, W., Wright, L. M., & Han, J.
(2006).
Rotational buoyancy effects on heat transfer in five different aspect-ratio rectangular channels with smooth walls and 45 degree ribbed walls. Journal of Heat Transfer.
1130-1141.
-
Mhetras, S., & Han, J.
(2006).
Effect of Superposition on Spanwise Film-Cooling Effectiveness Distribution on a Gas Turbine Blade. ASME -Publications- Htd.
477-487.
-
Suryanarayanan, A., Mhetras, S. R., Schobeiri, M. T., & Han, J. C.
(2006).
Film-cooling effectiveness on a rotating blade platform. 37-47.
-
Lau, S. C., Cervantes, J., Han, J. C., & Rudolph, R. J.
(2006).
Internal cooling near trailing edge of a gas turbine airfoil with cooling airflow through blockages with holes. 1005-1014.
-
Wright, L. M., Blake, S. A., & Han, J.
(2006).
Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows. ASME -Publications- Htd.
489-498.
-
Wright, L. M., Gao, Z., Yang, H., & Han, J.
(2006).
Film cooling effectiveness distribution on a gas turbine blade platform with inclined slot leakage and discrete film hole flows. 383-394.
-
Yang, H., Chen, H., & Han, J.
(2006).
Numerical study of a rotating blade platform with film cooling from cavity purge flow in a 1-% turbine stage. 315-324.
-
Liu, Y., Wright, L. M., Fu, W., & Han, J.
(2006).
Rib spacing effect on heat transfer and pressure loss in a rotating two-pass rectangular channel (AR=1:2) with 45-degree angled ribs. 363-373.
-
Yang, H. T., Chen, H. C., & Han, J. C.
(2006).
Turbine rotor with various tip configurations flow and heat transfer prediction. Journal of Thermophysics and Heat Transfer.
80-91.
-
Su, G., Chen, H., & Han, J.
(2005).
Computation of flow and heat transfer in rotating rectangular channels (AR=4 : 1) with pin-fins by a Reynolds stress turbulence model. 409-418.
-
Ahn, J., Schobeiri, M. T., Han, J., & Moon, H.
(2005).
Film cooling effectiveness on the leading edge of a rotating film-cooled blade using pressure sensitive paint. 375-384.
-
Mhetras, S., Yang, H., Gao, Z., & Han, J.
(2005).
Film-cooling effectiveness on squealer rim walls and squealer cavity floor of a gas turbine blade tip using pressure sensitive paint. 397-408.
-
Yang, H., Chen, H., Han, J., & Moon, H.
(2005).
Numerical prediction of film cooling and heat transfer on the leading edge of a rotating blade with two rows holes in a 1-(1)/(2) turbine stage at design and off design conditions. 335-344.
-
Gao, Z., Wright, L. M., & Han, J.
(2005).
Assessment of steady state PSP and transient IR measurement techniques for leading edge film cooling. ASME -Publications- Htd.
467-475.
-
Wright, L. M., Gao, Z., Varvel, T. A., & Han, J.
(2005).
Assessment of steady state PSP, TSP, and IR measurement techniques for flat plate film cooling. 37-46.
-
Fu, W., Wright, L. M., & Han, J.
(2005).
Buoyancy effects on heat transfer in five different aspect-ratio rectangular channels with smooth walls and 45-degree ribbed walls. 453-463.
-
Yang, H., Chen, H., & Han, J.
(2005).
Flow and Heat Transfer Prediction On Turbine Rotor Blade with Various Tip Configurations. 7551-7561.
-
Fu, W. L., Wright, L. M., & Han, J. C.
(2005).
Heat transfer in two-pass rotating rectangular channels (AR=1:2 and AR=1:4) with 45 deg angled rib turbulators. Journal of Turbomachinery.
164-174.
-
Su, G., Chen, H., Han, J., & Heidmann, J. D.
(2004).
Computation of Flow and Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:1, AR=1:2, AR=1:4) With 45-deg. Angled Ribs by Reynolds Stress Turbulence Model. 603-612.
-
Ahn, J., Schobeiri, M. T., Han, J., & Moon, H.
(2004).
Film Cooling Effectiveness on the Leading Edge of a Rotating Turbine Blade. ASME -Publications- Htd.
565-574.
-
Ahn, J., Mhetras, S., & Han, J.
(2004).
Film-Cooling Effectiveness on a Gas Turbine Blade Tip Using Pressure Sensitive Paint. 241-250.
-
Yang, H., Chen, H., & Han, J.
(2004).
Numerical Prediction of Film Cooling and Heat Transfer With Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade. 177-187.
-
Yang, H., Chen, H., Han, J., & Moon, H.
(2004).
Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade in a 1-1/2 Turbine Stage. ASME -Publications- Htd.
555-564.
-
Fu, W., Wright, L. M., & Han, J.
(2004).
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With 45 Angled Rib Turbulators. 305-315.
-
Fu, W., Wright, L. M., & Han, J.
(2004).
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=2:1) With Discrete V-Shaped and Discrete Angled Rib Turbulators. ASME -Publications- Htd.
545-554.
-
Wright, L. M., Fu, W., & Han, J.
(2004).
Thermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR = 4:1). 885-894.
-
Kwak, J. S., & Han, J. C.
(2003).
Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade. Journal of Turbomachinery.
648-657.
-
Kwak, J. S., Ahn, J., Han, J. C., Lee, C. P., Bunker, R. S., Boyle, R., & Gaugler, R.
(2003).
Heat transfer coefficients on the squealer tip and near-tip regions of a gas turbine blade with single or double squealer. Journal of Turbomachinery.
778-787.
-
Griffith, T. S., Al-Hadhrami, L., & Han, J. C.
(2003).
Heat transfer in rotating rectangular cooling channels (AR=4) with dimples. Journal of Turbomachinery.
555-563.
-
Kwak, J. S., & Han, J. C.
(2003).
Heat-transfer coefficients of a turbine blade-tip and near-tip regions. Journal of Thermophysics and Heat Transfer.
297-303.
-
Su, G., Teng, S., Chen, H., & Han, J.
(2003).
Computation of Flow and Heat Transfer in Rotating Rectangular Channels (AR = 4) With V-Shaped Ribs by a Reynolds Stress Turbulence Model. 237-246.
-
Kwak, J. S., Ahn, J., Han, J., Lee, C. P., Boyle, R., Gaugler, R., & Bunker, R. S.
(2003).
Heat Transfer Coefficients on the Squealer Tip and Near Tip Regions of a Gas Turbine Blade With Single or Double Squealer. 681-690.
-
Parsons, J. A., Han, J., & Lee, C. P.
(2003).
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Film Coolant Extraction. 671-680.
-
Wright, L. M., Lee, E., & Han, J.
(2003).
Effect of Rotation on Heat Transfer in Narrow Rectangular Cooling Channels (AR = 8:1 and 4:1) With Pin-Fins. 213-223.
-
Lee, E., Wright, L. M., & Han, J.
(2003).
Heat Transfer in Rotating Rectangular Channels (AR = 4:1) With V-Shaped and Angled Rib Turbulators With and Without Gaps. 661-670.
-
Al-Hadhrami, L. M., Griffith, T. S., & Han, J. C.
(2002).
Heat transfer in two-pass rotating rectangular channels (AR=2) with parallel and crossed 45 V-shaped rib turbulators
-
Azad, G. S., Uddin, M. J., Han, J. C., Moon, H. K., & Glezer, B.
(2002).
Heat transfer in a two-pass rectangular rotating channel with 45-deg angled rib turbulators. Journal of Turbomachinery.
251-259.
-
Al-Qahtani, M., Jang, Y. J., Chen, H. C., & Han, J. C.
(2002).
Prediction of flow and heat transfer in rotating two-pass rectangular channels with 45-deg rib turbulators. Journal of Turbomachinery.
242-250.
-
Al-Qahtani, M., Chen, H., & Han, J.
(2002).
A Numerical Study of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4) With 45 Rib Turbulators by Reynolds Stress Turbulence Model. 533-542.
-
Chen, H., & Han, J.
(2002).
Computation of Flow and Heat Transfer in Turbine Blade Cooling Passages by Reynolds Stress Turbulence Model (Keynote Paper). 867-883.
-
Kwak, J. S., & Han, J.
(2002).
Heat Transfer Coefficient on the Squealer Tip and Near Squealer Tip Regions of a Gas Turbine Blade. ASME -Publications- Htd.
245-254.
-
Griffith, T. S., Al-Hadhrami, L., & Han, J.
(2002).
Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Dimples. 551-560.
-
Kwak, J. S., & Han, J.
(2002).
Heat Transfer Coefficient and Film-Cooling Effectiveness on a Gas Turbine Blade Tip. 309-318.
-
Kwak, J. S., & Han, J.
(2002).
Heat Transfer Coefficient and Film-Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade. 1073-1082.
-
Kwak, J. S., Lee, J. H., & Han, J.
(2002).
Heat Transfer and Pressure Distributions on A Gas Turbine Vane End-Wall. 6.
-
Kwak, J. S., & Han, J. C.
(2002).
Heat transfer coefficient on the squealer tip and near squealer tip regions of a gas turbine blade. 245-254.
-
Han, J., Dutta, S., & Ekkad, S.
(2001).
Gas Turbine Heat Transfer and Cooling Technology. 1943-1946.
-
Azad, G. S., Han, J., Bunker, R. S., & Lee, C. P.
(2001).
Effect of Squealer Geometry Arrangement on Gas Turbine Blade Tip Heat Transfer. ASME -Publications- Htd.
297-305.
-
Teng, S., Han, J. C., & Poinsatte, P. E.
(2001).
Effect of film-hole shape on turbine-blade heat-transfer coefficient distribution. Journal of Thermophysics and Heat Transfer.
249-256.
-
Jang, Y. J., Chen, H. C., & Han, J. C.
(2001).
Computation of flow and heat transfer in two-pass channels with 60 deg ribs. Journal of Heat Transfer.
563-575.
-
Azad, G. S., Uddin, M. J., Han, J., Moon, H., & Glezer, B.
(2001).
Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45 Angled Rib Turbulators. v003t01a061-v003t01a061.
-
Al-Qahtani, M., Jang, Y., Chen, H., & Han, J.
(2001).
Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45 Rib Turbulators. v003t01a062-v003t01a062.
-
Han, J. C., & Dutta, S.
(2001).
Recent developments in turbine blade internal cooling. Annals of the New York Academy of Sciences.
162-178.
-
Jang, Y. J., Chen, H. C., & Han, J. C.
(2001).
Flow and heat transfer in a rotating square channel with 45 deg angled ribs by Reynolds stress turbulence model. Journal of Turbomachinery.
124-132.
-
Han, J., & Ekkad, S.
(2001).
Recent Development in Turbine Blade Film Cooling. International Journal of Rotating Machinery.
21-40.
-
Azad, G. S., Han, J. C., & Boyle, R. J.
(2000).
Float transfer and flow on the squealer tip of a gas turbine blade. Journal of Turbomachinery.
725-732.
-
Azad, G. S., Han, J. C., Teng, S. Y., & Boyle, R. J.
(2000).
Heat transfer and pressure distributions on a gas turbine blade tip. Journal of Turbomachinery.
717-724.
-
Jang, Y., Chen, H., & Han, J.
(2000).
Flow and Heat Transfer in a Rotating Square Channel With 45 Angled Ribs by Reynolds Stress Turbulence Model. v003t01a037-v003t01a037.
-
Azad, G. S., Han, J., & Boyle, R. J.
(2000).
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade. v003t01a003-v003t01a003.
-
Chen, H. C., Jang, Y. J., & Han, J. C.
(2000).
Near-wall second-moment closure for rotating multiple-pass cooling channels. Journal of Thermophysics and Heat Transfer.
201-209.
-
Teng, S. Y., Sohn, D. K., & Han, J. C.
(2000).
Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade. Journal of Turbomachinery.
340-347.
-
Chen, H., Wei, G., & Han, J.
(1999).
Computation of Discrete-Hole Film Cooling by a Near-Wall Second-Moment Turbulence Closure. ASME -Publications- Htd.
219-226.
-
Chen, H., Jang, Y., & Han, J.
(1999).
Assessment of a near-wall second-moment closure for rotating multiple-pass cooling channels
-
Chen, H., Jang, Y., & Han, J.
(1999).
Computation of Flow and Heat Transfer in Rotating Two-Pass Square Channels by a Reynolds Stress Model. v003t01a052-v003t01a052.
-
Teng, S., Sohn, D. K., & Han, J.
(1999).
Unsteady Wake Effect on Film Temperature and Effectiveness Distributions for a Gas Turbine Blade. v003t01a051-v003t01a051.
-
Akella, K. V., & Han, J. C.
(1998).
Impingement cooling in rotating two-pass rectangular channels. Journal of Thermophysics and Heat Transfer.
582-588.
-
Du, H., Ekkad, S. V., & Han, J.
(1998).
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade
-
Du, H., Ekkad, S. V., & Han, J.
(1998).
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade. American Society of Mechanical Engineers (Paper).
v004t09a057-v004t09a057.
-
Parsons, J. A., Han, J. C., & Lee, C. P.
(1998).
Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward crossflow. Journal of Turbomachinery.
79-85.
-
Sohn, D. K., Teng, S. Y., & Han, J. C.
(1998).
Film temperature and effectiveness measurements on a cylindrical leading edge film cooling model. 571-576.
-
Chandra, P. R., Fontenot, M. L., & Han, J. C.
(1998).
Effect of rib profiles on turbulent channel flow heat transfer. Journal of Thermophysics and Heat Transfer.
116-118.
-
Du, H., Han, J. C., & Ekkad, S. V.
(1997).
Detailed film cooling measurements over a gas turbine blade using a transient liquid crystal image technique. ASME -Publications- Htd.
245-254.
-
Du, H., Ekkad, S. V., & Han, J. C.
(1997).
Unsteady high turbulence effect on turbine blade film cooling heat transfer performance using a transient liquid crystal technique. NASA Conference Publication.
239-259.
-
Ekkad, S. V., Zapata, D., & Han, J. C.
(1997).
Heat transfer coefficients over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method. Journal of Turbomachinery.
580-586.
-
Ekkad, S. V., Han, J., & Du, H.
(1997).
Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density
-
Ekkad, S. V., Han, J., & Du, H.
(1997).
Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density. American Society of Mechanical Engineers (Paper).
v003t09a032-v003t09a032.
-
Du, H., Han, J., & Ekkad, S. V.
(1997).
Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade
-
Du, H., Han, J., & Ekkad, S. V.
(1997).
Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade. American Society of Mechanical Engineers (Paper).
v003t09a031-v003t09a031.
-
Akella, K., Han, J., Akella, K., & Han, J.
(1997).
Jet impingement cooling in rotating two-pass rectangular channels with smooth walls
-
Chandra, P. R., Niland, M. E., & Han, J. C.
(1997).
Turbulent flow heat transfer and friction in a rectangular channel with varying numbers of ribbed walls. Journal of Turbomachinery.
374-380.
-
Du, H., Ekkad, S., & Han, J. C.
(1996).
Effect of unsteady wake with trailing edge coolant ejection on detailed heat transfer coefficient distributions for a gas turbine blade. ASME -Publications- Htd.
81-88.
-
Parsons, J. A., & Han, J. C.
(1996).
Rotation effect on jet impingement heat transfer in smooth rectangular channels with heated target walls and film coolant extraction. American Society of Mechanical Engineers (Paper).
-
Chandra, P., Fontenot, M., & Han, J.
(1996).
Effect of non-traditional rib-profiles on heat transfer and friction in turbulent channel flows
-
Dutta, S., Andrews, M. J., & Han, J.
(1996).
Prediction of Turbulent Flow and Heat Transfer in Rotating Square and Rectangular Smooth Channels. v004t09a031-v004t09a031.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1996).
Prediction of turbulent flow and heat transfer in rotating square and rectangular smooth channels. American Society of Mechanical Engineers (Paper).
-
Parsons, J. A., Han, J. C., & Lee, C. P.
(1996).
Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward cross flow. American Society of Mechanical Engineers (Paper).
-
Ekkad, S. V., Du, H., & Han, J. C.
(1995).
Local heat transfer coefficient and film effectiveness distributions on a cylindrical leading edge model using a transient liquid crystal image method. American Society of Mechanical Engineers (Paper).
-
Ekkad, S. V., Zapata, D., & Han, J.
(1995).
Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method
-
Ekkad, S. V., Zapata, D., & Han, J.
(1995).
Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method. American Society of Mechanical Engineers (Paper).
v004t09a011-v004t09a011.
-
Ekkad, S. V., Zapata, D., & Han, J.
(1995).
Heat Transfer Coefficients Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method. v004t09a010-v004t09a010.
-
Chandra, P. R., Niland, M. E., & Han, J.
(1995).
Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Number of Ribbed Walls
-
Chandra, P. R., Niland, M. E., & Han, J.
(1995).
Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Number of Ribbed Walls. American Society of Mechanical Engineers (Paper).
v004t09a013-v004t09a013.
-
Dutta, S., Andrews, M. J., & Han, J. C.
(1994).
Numerical prediction of turbulent heat transfer in a rotating square duct with variable rotational buoyancy effects. ASME -Publications- Htd.
161-170.
-
OU, S., HAN, J. C., MEHENDALE, A. B., & LEE, C. P.
(1994).
UNSTEADY WAKE OVER A LINEAR TURBINE BLADE CASCADE WITH AIR AND CO2 FILM INJECTION .1. EFFECT ON HEAT-TRANSFER COEFFICIENTS. Journal of Turbomachinery.
721-729.
-
Dutta, S., Han, J. C., Zhang, Y., & Lee, C. P.
(1994).
Local heat transfer in a rotating two-pass triangular duct with smooth walls
-
Dutta, S., Han, J. C., Zhang, Y., & Lee, C. P.
(1994).
Local heat transfer in a rotating two-pass triangular duct with smooth walls. American Society of Mechanical Engineers (Paper).
1-11.
-
Zhang, L., & Han, J. C.
(1993).
Influence of mainstream turbulence on heat transfer coefficients from a gas turbine blade. ASME -Publications- Htd.
33-40.
-
Ou, S., & Han, J. C.
(1993).
Unsteady wake effect on film effectiveness and heat transfer coefficient from a turbine blade with one row of air and CO
2 film injection. American Society of Mechanical Engineers (Paper). 1-8.
-
Kim, S. Y., Han, J. C., Morrison, G. L., & Elovic, E.
(1993).
Influence of Surface Heating Condition on Local Heat Transfer in Enclosed Corotating Disks With Axial Throughflow. v03bt16a014-v03bt16a014.
-
Zhang, Y. M., Han, J. C., Parsons, J. A., & Lee, C. P.
(1993).
Surface Heating Effect on Local Heat Transfer in a Rotating Two-Pass Square Channel With 60 Angled Rib Turbulators. v03bt16a092-v03bt16a092.
-
Ou, S., Han, J., Mehendale, A. B., & Lee, C. P.
(1993).
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part I Effect on Heat Transfer Coefficients. v03at15a061-v03at15a061.
-
Mehendale, A. B., Han, J., Ou, S., & Lee, C. P.
(1993).
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II Effect on Film Effectiveness and Heat Transfer Distributions
-
Mehendale, A. B., Han, J., Ou, S., & Lee, C. P.
(1993).
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II Effect on Film Effectiveness and Heat Transfer Distributions. American Society of Mechanical Engineers (Paper).
v002t08a013-v002t08a013.
-
Kim, S. Y., Han, J. C., & Morrison, G. L.
(1993).
Influence of surface heating condition on local heat transfer in enclosed corotating disks with axial throughflow. American Society of Mechanical Engineers (Paper).
1-7.
-
Zhang, Y. M., Han, J. C., Parsons, J. A., & Lee, C. P.
(1993).
Surface heating effect on local heat transfer in a rotating two-pass square channel with 60 angled rib turbulators. American Society of Mechanical Engineers (Paper).
1-9.
-
Ou, S., Han, J. C., & Mehendale, A. B.
(1993).
Unsteady wake over a linear turbine blade cascade with air co film injection: Part I - effect on heat transfer coefficients. American Society of Mechanical Engineers (Paper).
-
MEHENDALE, A. B., & HAN, J. C.
(1992).
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE FILM COOLING HEAT-TRANSFER - EFFECT OF FILM HOLE SPACING. International Journal of Heat and Mass Transfer.
2593-2604.
-
HAN, J. C., ZHANG, Y. M., & LEE, C. P.
(1992).
INFLUENCE OF SURFACE HEAT-FLUX RATIO ON HEAT-TRANSFER AUGMENTATION IN SQUARE CHANNELS WITH PARALLEL, CROSSED, AND V-SHAPED ANGLED RIBS. Journal of Turbomachinery.
872-880.
-
Ou, S., & Han, J. C.
(1992).
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots. Journal of Turbomachinery.
724-733.
-
Han, J. C., Zhang, Y. M., & Lee, C. P.
(1992).
Influence of Surface Heating Condition on Local Heat Transfer in a Rotating Square Channel With Smooth Walls and Radial Outward Flow. v004t09a005-v004t09a005.
-
Ou, S., & Han, J. C.
(1991).
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots. American Society of Mechanical Engineers (Paper).
v004t09a013-v004t09a013.
-
Han, J. C., Zhang, Y. M., & Lee, C. P.
(1991).
Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed and V-Shaped Angled Ribs. American Society of Mechanical Engineers (Paper).
v004t09a002-v004t09a002.
-
LAU, S. C., MCMILLIN, R. D., & HAN, J. C.
(1991).
HEAT-TRANSFER CHARACTERISTICS OF TURBULENT-FLOW IN A SQUARE CHANNEL WITH ANGLED DISCRETE RIBS. Journal of Turbomachinery.
367-374.
-
HAN, J. C., & ZHANG, P.
(1991).
EFFECT OF RIB-ANGLE ORIENTATION ON LOCAL MASS-TRANSFER DISTRIBUTION IN A 3-PASS RIB-ROUGHENED CHANNEL. Journal of Turbomachinery.
123-130.
-
Lau, S. C., McMillin, R. D., & Han, J. C.
(1990).
Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs
-
Lau, S. C., McMillin, R. D., & Han, J. C.
(1990).
Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs. American Society of Mechanical Engineers (Paper).
v004t09a029-v004t09a029.
-
Mehendale, A. B., & Han, J. C.
(1990).
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer. American Society of Mechanical Engineers (Paper).
v004t09a002-v004t09a002.
-
Mehendale, A. B., & Han, J. C.
(1990).
Influence of high mainstream turbulence on leading edge film cooling heat transfer
-
Mehendale, A. B., Han, J. C., & Ou, S.
(1990).
Influence of high mainstream turbulence on leading edge heat transfer. ASME -Publications- Htd.
27-35.
-
Han, J. C., & Zhang, P.
(1989).
Effect of rib-angle orientation on local mass transfer distribution in a three-pass rib-roughened channel. American Society of Mechanical Engineers (Paper).
-
Lau, S. C., McMillin, R. D., & Han, J. C.
(1989).
Turbulent heat transfer and friction in a square channel with discrete rib turbulators. ASME -Publications- Htd.
33-41.
-
Han, J. C., & Zhang, P.
(1989).
Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel. v004t08a010-v004t08a010.
-
Lau, S. C., Han, J. C., & Batten, T.
(1989).
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes. Journal of Turbomachinery.
116-123.
-
Young, C. D., & Han, J. C.
(1988).
Effect of jet grid turbulence on turbulent boundary layer heat transfer. ASME -Publications- Htd.
37-44.
-
HAN, J. C., CHANDRA, P. R., & LAU, S. C.
(1988).
LOCAL HEAT MASS-TRANSFER DISTRIBUTIONS AROUND SHARP 180 DEG TURNS IN 2-PASS SMOOTH AND RIB-ROUGHENED CHANNELS. Journal of Heat Transfer.
91-98.
-
Kim, Y. S., Lau, S. C., & Han, J. C.
(1987).
LOCAL ENDWALL HEAT/MASS TRANSFER AND PRESSURE DROP IN A PIN FIN CHANNEL WITH LATERAL FLOW EJECTION. ASME -Publications- Htd.
95-102.
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1987).
EFFECT OF LATERAL FLOW EJECTION ON TURBULENT HEAT TRANSFER IN PIN FIN CHANNELS. ASME -Publications- Htd.
27-34.
-
Lau, S. C., Ong, L. E., & Han, J. C.
(1987).
Forced convective heat transfer in channels with internal longitudinal fins
-
Han, J. C., & Fletcher, L. S.
(1987).
INFLUENCE OF CONCURRENT STEAM SHEAR VELOCITY ON FALLING FILM EVAPORATION AND BOILING ON A HORIZONTAL TUBE. 527-532.
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1987).
LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL. 64-75.
-
Han, J. C., Chandra, P. R., & Lau, S. C.
(1987).
LOCAL HEAT/MASS TRANSFER DISTRIBUTION AROUND SHARP 180 degree TURN IN A SMOOTH SQUARE CHANNEL. 54-63.
-
Han, J., & Park, J. S.
(1986).
LOCAL HEAT TRANSFER AUGMENTATION IN CHANNELS WITH TWO OPPOSITE RIBBED SURFACES. 2885-2890.
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1985).
EFFECTS OF FIN CONFIGURATION AND ENTRANCE LENGTH ON LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL. American Society of Mechanical Engineers (Paper).
-
Lau, S. C., Kim, Y. S., & Han, J. C.
(1985).
EFFECTS OF FIN CONFIGURATION AND ENTRANCE LENGTH ON LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL. American Society of Mechanical Engineers (Paper).
-
HAN, J. C., PARK, J. S., & LEI, C. K.
(1985).
HEAT-TRANSFER ENHANCEMENT IN CHANNELS WITH TURBULENCE PROMOTERS. Journal of Engineering for Gas Turbines and Power.
628-635.
-
Lee, C. P., & Han, J. C.
(1983).
APPLICATION OF ADIABATIC FILM COOLING EFFECTIVENESS TO NON-ADIABATIC BLADE COOLING DESIGN. American Society of Mechanical Engineers (Paper).
-
Conklin, G. E., Han, J. C., & Jenkins, P. E.
(1983).
Film Cooling With Steam Injection Through Three Staggered Rows of Inclined Holes Over a Straight Airfoil. American Society of Mechanical Engineers (Paper).
v004t09a002-v004t09a002.
-
Han, J. C., Chen, H. W., & Jenkins, P. E.
(1983).
HEAT TRANSFER AND FILM COOLING WITH STEAM INJECTION THROUGH AN INCLINED HOLE OVER A FLAT PLATE. American Society of Mechanical Engineers (Paper).
-
Han, J. C., & Lei, C. K.
(1983).
HEAT TRANSFER AND FRICTION IN SQUARE DUCTS WITH TWO OPPOSITE RIB-ROUGHENED WALLS. American Society of Mechanical Engineers (Paper).
-
LEE, C. P., & HAN, J. C.
(1983).
THE APPLICATION OF ADIABATIC FILM COOLING EFFECTIVENESS TO NON-ADIABATIC BLADE COOLING DESIGN. Mechanical Engineering.
104-104.
-
Han, J. C., Ortman, D. W., & Lee, C. P.
(1982).
COMPUTER MODEL FOR GAS TURBINE BLADE COOLING ANALYSIS. American Society of Mechanical Engineers (Paper).
-
Han, J. C., Ortman, D. W., & Lee, C. P.
(1982).
A Computer Model for Gas Turbine Blade Cooling Analysis. v001t01a006-v001t01a006.
-
Han, J., & Jenkins, P. E.
(1982).
Prediction of Film Cooling Effectiveness of Steam. v004t09a003-v004t09a003.
-
Han, J. C., & Jenkins, P. E.
(1982).
PREDICTION OF FILM COOLING EFFECTIVENESS OF STEAM. American Society of Mechanical Engineers (Paper).
-
Chowdhury, N., Shiau, C., Han, J., Xu, H., & Fox, M.
(2018).
FILM COOLING EFFECTIVENESS COMPARISON ON TURBINE VANE ENDWALL WITH CLUSTER CONFIGURATIONS USING PSP MEASUREMENT TECHNIQUE. v008t10a039-v008t10a039.
-
patent
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2010).
Plasma lifted boundary layer gas turbine engine vane
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2010).
Plasma induced virtual turbine airfoil trailing edge extension
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2010).
Downstream plasma shielded film cooling
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2009).
Airfoil leading edge end wall vortex reducing plasma
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2009).
Upstream plasma shielded film cooling
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2008).
Airfoil with plasma generator at leading edge for vortex reduction and corresponding operating method
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2008).
Airfoil with plasma generator for shielding a boundary layer downstream of a film cooling hole and corresponding operating method
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2008).
Airfoil with plasma generator for shielding a boundary layer upstream of a film cooling hole and corresponding operating method
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2008).
Airfoil with plasma generator on trailing edge and corresponding operating method
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2008).
Plasma boundary layer lifting systems for a gas turbine engine vane and corresponding method for operating a gas turbine engine
-
Hendry, J. W., & Han, J. C.
(1983).
Method and apparatus for heating a mold cavity uniformly
-
Lee, C. P., Wadia, A. R., Cherry, D. G., & Han, J. C.
(2010).
Plasma lifted boundary layer gas turbine engine vane
-
report
-
Han, J. C., Park, J. S., & Ibrahim, M. Y.
(1986).
MEASUREMENT OF HEAT TRANSFER AND PRESSURE DROP IN RECTANGULAR CHANNELS WITH TURBULENCE PROMOTERS. NASA contractor report. NASA CR. United States. National Aeronautics and Space Administration.
-
Han, J. C., Park, J. S., & Lei, C. K.
(1984).
HEAT TRANSFER AND PRESSURE DROP IN BLADE COOLING CHANNELS WITH TURBULENCE PROMOTERS. NASA contractor report. NASA CR. United States. National Aeronautics and Space Administration.
-
Han, J. C., Park, J. S., & Ibrahim, M. Y.
(1986).
MEASUREMENT OF HEAT TRANSFER AND PRESSURE DROP IN RECTANGULAR CHANNELS WITH TURBULENCE PROMOTERS. NASA contractor report. NASA CR. United States. National Aeronautics and Space Administration.
Teaching
teaching activities
- MEEN461 Heat Transfer Instructor
- MEEN628 Heat Trans-convec Instructor
- MEEN630 Intermed Heat Transfer Instructor
- MEEN642 Gas Turbine Ht Transfer Instructor
- MEEN643 Exp Meth Heat & Fld Mech Instructor
- MEEN684 Professional Internship Instructor
- MEEN684 Professional Internship Instructor
- MEEN685 Directed Studies Instructor
- MEEN691 Research Instructor
Works By Students
chaired theses and dissertations
-
Ahn, Jaeyong (2005-12). Film cooling effectiveness measurements on rotating and non-rotating turbine components.
-
Alkhamis, Nawaf Yahya (2010-10). Heat Transfer and Pressure Drop Measurement for Square Channels with V-shape Ribs at High Reynolds Numbers.
-
Bashir, Muhammad Hassan (2016-07). Film Cooling Effectiveness for Three Row Compound Hole Design on Flat Plate Using PSP Technique.
-
Blake, Sarah Anne (2007-05). Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex.
-
Chen, Andrew F (2013-11). Film Cooling with Forward and Backward Injection for Cylindrical and Fan-shaped Holes Using PSP Measurement Technique.
-
Chen, Andrew F (2018-04). Turbine Platform Film Cooling Effectiveness and Rotational Effect on Internal Cooling Passages with a Converging Tip Turn.
-
Choi, Jungho (2004-12). An experimental investigation of turbine blade heat transfer and turbine blade trailing edge cooling.
-
Chowdhury, MD Nafiz Hossain Khan (2017-05). Measurements and Assessment of Adiabatic Film Cooling Performance on a Gas Turbine Vane Endwall Using PSP Technique.
-
Chu, Hung-Chieh 1979- (2012-11). Numerical Simulation of Flow and Heat Transfer in Internal Multi-Pass Cooling Channel within Gas Turbine Blade.
-
Fu, Wen-Lung (2005-05). Aspect ratio effect on heat transfer in rotating two-pass rectangular channels with smooth walls and ribbed walls.
-
Gao, Zhihong (2009-05). Experimental investigation of film cooling effectiveness on gas turbine blades.
-
Grizzle, Joshua Peter Fletcher (2009-05). Film cooling on a flat plate: investigating density.
-
Huh, Michael (2010-01). Heat Transfer in Smooth and Ribbed Rectangular Two-Pass Channels with a Developing Flow Entrance at High Rotation Numbers.
-
Krad, Belal (2013-11). Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques.
-
Lane, Matthew Ryan (2013-07). Experimental and Numerical Investigation on Fouling Parameters in a Small-Scale Rotating Unit.
-
Lee, Jiyeon (2015-09). The Effect of Mainstream Turbulence on Turbine Blade Platform Cooling with Simulated Swirl Purge Flow.
-
Lei, Jiang 1980- (2011-08). Heat Transfer in Rectangular Channels (AR=2:1) of the Gas Turbine Blade at High Rotation Numbers.
-
Li, Shiou-Jiuan (2012-12). Experimental Investigation of Film Cooling Effectiveness on Gas Turbine Blades.
-
Liu, Kevin (2012-10). Parametric Study of Gas Turbine Film-Cooling.
-
Liu, Kuo-Chun (2010-01). Blowing Ratio Effects on Film Cooling Effectiveness.
-
Liu, Yao-Hsien (2005-08). Effect of rib spacing on heat transfer and friction in a rotating two-pass rectangular (AR=1:2) channel.
-
Liu, Yao-Hsien (2008-12). Heat transfer in leading and trailing edge cooling channels of the gas turbine blade under high rotation numbers.
-
Lu, Kun (2014-12). Numerical Investigations of Flow and Film Cooling with Endwall Contouring and Blade Tip Ejection under Rotating Turbine Conditions.
-
Mhetras, Shantanu (2009-06). Experimental study of gas turbine blade film cooling and internal turbulated heat transfer at large Reynolds numbers.
-
Narzary, Diganta P. (2010-10). Experimental Study of Gas Turbine Blade Film Cooling and Heat Transfer.
-
Nuntakulamarat, Metapun (2018-07). HEAT TRANSFER AND PRESSURE DROP MEASUREMENTS IN LOW ASPECT RATIO CHANNELS WITH CIRCULAR PINS AND STRIP FINS.
-
Qureshi, Shamsul Arfin (2017-01). Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique.
-
Rallabandi, Akhilesh P. (2010-10). Parametric Study of Turbine Blade Internal Cooling and Film Cooling.
-
Rezasoltani, Mohsen (2015-12). Experimental Investigations of Flow and Film Cooling with Endwall Contouring and Blade Tip Ejection under Rotating Turbine Conditions.
-
Su, Guoguang (2005-12). Numerical simulation of flow and heat transfer of internal cooling passage in gas turbine blade.
-
Ullah, Izhar (2018-07). Flat Plate Film Cooling with Linear and Curved Round-to-Diffusion Shaped Slots Using PSP Measurement Technique.
-
Ullah, Izhar (2018-07). Flat Plate Film Cooling with Linear and Curved Round-to-Diffusion Shaped Slots Using PSP Measurement Technique.
-
Varvel, Trent Alan (2004-12). Shaped hole effects on film cooling effectiveness and a comparison of multiple effectiveness measurement techniques.
-
Wang, Nian (2018-12). Turbine Blade Internal Heat Transfer and Film Cooling Studies.
-
Wright, Lesley Mae (2009-06). Experimental investigation of turbine blade platform film cooling and rotational effect on trailing edge internal cooling.
-
Yang, Shangfeng (2014-12). Turbine Vane Film Cooling and Internal Rotating Coolant Passage Heat Transfer.
-
Zhang, Mingjie (2018-11). Experimental and Numerical Investigation of Turbine Blade Leading Edge Heat Transfer with Jet Impingement and Film Cooling.
-
Zirakzadeh, Hootan (2014-08). Numerical Investigation of Temperature Distribution on a High Pressure Gas Turbine Blade.
Background
awards and honors
- AAAS Fellow, conferred by American Association For The Advancement of Science - (Washington D.C., District of Columbia, United States), 2023
- AIAA Fellow, conferred by American Institute of Aeronautics and Astronautics - (Reston, Virginia, United States), 2016
- Max Jakob Memorial Award, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2016
- ASME IGTI Aircraft Engine Technology Award, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2016
- ASME Heat Transfer Division 75th Anniversary Medal, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2013
- ASME K-14 Warren Rohsenow Prize for Best Presentation, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2007
- University Distinguished Professor, conferred by Texas A&M University - (College Station, Texas, United States), 2006
- Thermophysics Award, conferred by American Institute of Aeronautics and Astronautics - (Reston, Virginia, United States), 2004
- ASME IGTI Certificate Award for Valued Service as Chair of the Heat Transfer Committee, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2004
- Heat Transfer Memorial Award, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2002
- Fellow, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 1991
Contact
first name
- Je-Chin
has last name
- Han
mailing address
-
Texas A&M University
Mechanical Engineering
3123 TAMU
College Station, TX 77843-3123
USA
Other
- jc-han@tamu.edu