HR job title
- Director Hypersonic Facilities
- Contact Info
- 1 979 845 8170
- ORCiD
- 0000-0001-9500-2719
Tichenor, Nathan Research Assistant Professor
Positions
- Director of Hypersonic Facilities, Bush Combat Development Complex, Texas A&M Engineering Experiment Station (TEES), Texas A&M University
- Research Assistant Professor, Aerospace Engineering, College of Engineering
- Overview
- Publications
- Teaching
- Background
- Contact
- Other
- View All
Overview
Publications
selected publications
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academic article
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Leidy, A. N., Neel, I. T., Tichenor, N. R., Bowersox, R., & Schmisseur, J. D.
(2021).
Tunnel Noise Effects on Hypersonic Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interactions. AIAA Journal: devoted to aerospace research and development.
59(7), 1-11.
-
McElreath, J. W., Benedict, M., & Tichenor, N.
(2020).
Cycloidal Rotor-Blade Tip-Vortex Analysis at Low Reynolds Number. AIAA Journal: devoted to aerospace research and development.
58(6), 2560-2570.
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Leidy, A. N., Neel, I. T., Tichenor, N. R., & Bowersox, R.
(2020).
High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave-Boundary-Layer Interactions. AIAA Journal: devoted to aerospace research and development.
58(7), 3090-3099.
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Bright, A., Tichenor, N., Kremeyer, K., & Wlezien, R.
(2018).
Boundary-Layer Separation Control Using Laser-Induced Air Breakdown. AIAA Journal: devoted to aerospace research and development.
56(4), 1-11.
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Bright, A., Tichenor, N., Kremeyer, K., & Wlezien, R
(2018).
Boundary-layer separation control using laser-induced air breakdown. AIAA Journal: devoted to aerospace research and development.
56(4), 1472-1482.
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Tichenor, N. R
(2017).
Hypervelocity Research Tunnel for Fundamental High-Enthalpy Research
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Long, R. R., White, E. B., Tichenor, N. R., & Kremeyer, K.
(2017).
Instantaneous Wind-Tunnel Model Vibration Measurements Using a Kalman Filtering Approach. Journal of Fluids Engineering.
139(7), 071106.
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Tichenor, N. R., Humble, R. A., & Bowersox, R.
(2013).
Response of a hypersonic turbulent boundary layer to favourable pressure gradients. Journal of Fluid Mechanics.
722, 187-213.
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Kobayashi, K., Bowersox, R., Srinivasan, R., Tichenor, N. R., Carter, C. D., & Ryan, M. D.
(2010).
Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow. Journal of Propulsion and Power: devoted to aerospace propulsion and power.
26(2), 373-376.
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Leidy, A. N., Neel, I. T., Tichenor, N. R., Bowersox, R., & Schmisseur, J. D.
(2021).
Tunnel Noise Effects on Hypersonic Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interactions. AIAA Journal: devoted to aerospace research and development.
59(7), 1-11.
-
conference paper
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Carlson, J., Bowersox, R. D., & Tichenor, N. R.
(2020).
Proper Orthogonal Decomposition Analysis of Hypersonic Turbulent Boundary Layers Subjected to Streamline Wall Curvature. 2060.
-
Leidy, A., Neel, I. T., Tichenor, N. R., Bowersox, R. D., & Schmisseur, J. D.
(2020).
Some effects of tunnel noise on cylinder-induced Mach 6 transitional shock wave boundary layer interactions. 0582.
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Tichenor, N. R., Leiweke, R., & Ombrello, T.
(2020).
Towards Supersonic Flat-Wall Flame Holding with Nanosecond-Pulsed High-Frequency Discharges. 1431.
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Tichenor, N. R., Leiweke, R. J., & Ombrello, T.
(2019).
Effects of Fuel Mixture Properties on Nanosecond Pulsed High Frequency Discharge Ignition
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Mabe, J. H., Hartl, D. J., Tichenor, N., Zackery, M., Blades, E., & Nucci, M.
(2019).
Fluid-Structure Interaction Modeling of a Shape-Memory Alloy Actuated Supersonic Wind Tunnel Model Alloy. 0602.
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Tichenor, N. R., Leiweke, R., & Ombrello, T.
(2019).
Investigation of Partially-Coupled Ignition Using Nanosecond Pulsed High Frequency Discharges. 3116.
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Santiago, J., Tichenor, N., & Araya, G
(2019).
Thermal transport in hypersonic turbulent boundary layers at high-Reynolds numbers. G11-007.
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Tichenor, N. R.
(2019).
Turbulent / Non-Turbulent Interface and Uniform Momentum Zones of High-Speed Turbulent Boundary Layers Subjected to Streamline Pressure Gradient. 3341.
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Neel, I. T., Leidy, A., Tichenor, N. R., & Bowersox, R.
(2018).
Characterization of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone
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Leidy, A., Neel, I. T., Tichenor, N. R., Bowersox, R., & Schmisseur, J. D.
(2018).
Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading
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Leidy, A., Neel, I. T., Tichenor, N. R., Bowersox, R. D., & Schmisseur, J. D.
(2018).
High-Speed Schlieren Imaging and Hot-wire Characterization of Cylinder-Induced Hypersonic Shock Boundary Layer Interactions
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Neel, I. T., Leidy, A., Tichenor, N. R., & Bowersox, R. D.
(2018).
Influence of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone
-
McElreath, J. W., Benedict, M., & Tichenor, N.
(2018).
Tip vortex measurements on a cycloidal rotor blade at ultralow Reynolds numbers. Annual Forum Proceedings - AHS International.
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Tichenor, N. R., Neel, I., Leidy, A., & Bowersox, R. D.
(2017).
Influence of Streamline Adverse Pressure Gradients on the Structure of a Mach 5 Turbulent Boundary Layer
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Neel, I. T., Leidy, A., Bowersox, R. D., & Tichenor, N. R.
(2016).
Hypersonic Boundary Layer with Streamline Curvature-Driven Adverse Pressure Gradient
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Bright, A. V., Tichenor, N. R., & Wlezien, R.
(2015).
The Effects of Laser Plasma Discharge on a Separating Boundary Layer. 1960.
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Tichenor, N., Bright, A., Kremeyer, K., Lenzner, M., Yeak, J., & Wlezien, R.
(2013).
Experimental Investigation of Laser-Based Flow Modification Over a Low Speed Airfoil. 903.
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Tichenor, N., Humble, R., & Bowersox, R.
(2012).
Reynolds Stresses in a Hypersonic Boundary Layer with Streamline Curvature-Driven Favorable Pressure Gradients
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Tichenor, N., Humble, R., & Bowersox, R.
(2011).
Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer. 748.
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Tichenor, N., Semper, M., Bowersox, R., Srinvasan, R., & North, S.
(2010).
Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel
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Kobayashi, K., Bowersox, R., Srinivasan, R., Tichenor, N., Carter, C., & Ryan, M.
(2009).
Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow
-
Kobayashi, K., Bowersox, R., Srinivasan, R., Tichenor, N. R., Carter, C. D., & Ryan, M. D.
(2009).
Experimental and numerical studies of diamond-shaped injector in a supersonic flow
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Semper, M., Tichenor, N., Bowersox, R., Srinvasan, R., & North, S.
(2009).
On the Design and Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel
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Carlson, J., Bowersox, R. D., & Tichenor, N. R.
(2020).
Proper Orthogonal Decomposition Analysis of Hypersonic Turbulent Boundary Layers Subjected to Streamline Wall Curvature. 2060.
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report
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Rediniotis, O., Bowersox, R., Kirk, A., Kumar, A., & Tichenor, N
(2007).
Active control of jet engine inlet flows
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Rediniotis, O., Bowersox, R., Kirk, A., Kumar, A., & Tichenor, N
(2007).
Active control of jet engine inlet flows
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thesis
Teaching
teaching activities
- AERO302 Aero Engr Lab Instructor
- AERO491 Hnr-research Instructor
- AERO691 Research Instructor
Background
education and training
- Ph.D. in Aerospace Engineering, Texas A&M University - (College Station, Texas, United States) 2010
- M.S. in Aerospace Engineering, Texas A&M University - (College Station, Texas, United States) 2007
- B.S. in Aerospace Engineering, Texas A&M University - (College Station, Texas, United States) 2005
Contact
first name
- Nathan
has last name
- Tichenor
mailing address
-
Texas A&M Engineering Experiment Station
Aerospace Engineering
3141 TAMUS
College Station, TX 77843-3141
USA
Other
- ntichenor@tamu.edu