HR job title
- Professor
- Contact Info
- 1 979 845 5952
- ORCiD
- 0000-0001-8785-3038
Cizmas, Paul Professor
Positions
- Professor, Aerospace Engineering, College of Engineering
- Faculty Affiliate, The Turbomachinery Laboratory, Texas A&M Engineering Experiment Station (TEES)
- Faculty Affiliate, Energy Institute, Texas A&M Engineering Experiment Station (TEES)
Research Areas
- Overview
- Publications
- Research
- Teaching
- Works By Students
- Background
- Contact
- Other
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Overview
Publications
selected publications
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academic article
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Han, Z., & Cizmas, P.
A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors. International Journal of Turbo and Jet Engines.
20(1), 1-16.
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Cizmas, P. G., & Strganac, T. W.
A Novel Method for Prediction of Nonlinear Aeroelastic Responses
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Cizmas, P., & Subramanya, R.
A Parallel Algorithm for Simulation of Unsteady Flows in Multistage Turbomachinery. International Journal of Turbo and Jet Engines.
18(2), 117-132.
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Freno, B. A., & Cizmas, P.
A computationally efficient non-linear beam model. International Journal of Non-Linear Mechanics.
46(6), 854-869.
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Ream, A. E., Slattery, J. C., & Cizmas, P.
A method for generating reduced-order combustion mechanisms that satisfy the differential entropy inequality. Physics of Fluids.
30(4), 043601.
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Guarnieri, J. A., & Cizmas, P. G.
A method for reducing jet engine thermal signature. International Journal of Turbo and Jet Engines.
25(1), 1-11.
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Schoppe, J., & Cizmas, P.
A multi-limiter method for simulating complex flows on large grids. Physics of Fluids.
35(12), 125115.
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Freno, B. A., & Cizmas, P.
A proper orthogonal decomposition method for nonlinear flows with deforming meshes. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW.
50, 145-159.
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Ream, A. E., Slattery, J. C., & Cizmas, P.
A reduced-order methane-air combustion mechanism that satisfies the differential entropy inequality. Proceedings of the Romanian Academy Series A - Mathematics Physics Technical Sciences Information Science.
19, 285-290.
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Yuan, T., Cizmas, P. G., & O'Brien, T.
A reduced-order model for a bubbling fluidized bed based on proper orthogonal decomposition. Computers and Chemical Engineering.
30(2), 243-259.
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Brenner, T. A., Fontenot, R. L., Cizmas, P., OBrien, T. J., & Breault, R. W.
A reduced-order model for heat transfer in multiphase flow and practical aspects of the proper orthogonal decomposition. Computers and Chemical Engineering.
43, 68-80.
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Cizmas, P., Richardson, B. R., Brenner, T. A., OBrien, T. J., & Breault, R. W.
Acceleration techniques for reduced-order models based on proper orthogonal decomposition. Journal of Computational Physics.
227(16), 7791-7812.
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Krath, E. H., Carpenter, F. L., Cizmas, P., & Johnston, D. A.
An efficient proper orthogonal decomposition based reduced-order model for compressible flows. Journal of Computational Physics.
426, 109959-109959.
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Freno, B. A., & Cizmas, P.
An investigation into the significance of the non-linear terms in the equations of motion for a cantilevered beam. International Journal of Non-Linear Mechanics.
47(3), 84-95.
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Brenner, T. A., Fontenot, R. L., Cizmas, P., O'Brien, T. J., & Breault, R. W.
Augmented proper orthogonal decomposition for problems with moving discontinuities. Powder Technology.
203(1), 78-85.
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Cizmas, P., & Hall, K. C.
Computation Of Steady and Unsteady Viscous Flows Using a Simultaneously Coupled Inviscid-Viscous Interaction Technique. Journal of Fluids and Structures.
9(6), 639-657.
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Reddy, S. R., Freno, B. A., Cizmas, P., Gokaltun, S., McDaniel, D., & Dulikravich, G. S.
Constrained reduced-order models based on proper orthogonal decomposition. Computer Methods in Applied Mechanics and Engineering.
321, 18-34.
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Jones, N. H., Cizmas, P., & Slattery, J. C.
Creating Reduced Kinetics Models That Satisfy the Entropy Inequality. Journal of Engineering for Gas Turbines and Power.
137(7), 071504.
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Cizmas, P. G., & Slattery, J. C.
Dimensionless correlation for sand erosion of families of polymers. Wear.
262(3-4), 316-319.
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Dorney, D. J., Sondak, D. L., & Cizmas, P. G.
Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine. International Journal of Turbo and Jet Engines.
17(2), 119-131.
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Johnson, S., Carpenter, F. L., Rediniotis, O. K., & Cizmas, P.
Experimental Validation of a Pulse-Modulated Flow-Control Actuator for Turbomachinery. Journal of Propulsion and Power.
33(6), 1358-1368.
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Palacios, A., Finney, C., Cizmas, P., Daw, S., & O'Brien, T.
Experimental analysis and visualization of spatiotemporal patterns in spouted fluidized beds. Chaos.
14(2), 499-509.
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MCCRAY, M. C., & CIZMAS, P.
Experimental investigation of the critical Reynolds number for bubbly two-phase flow. INCAS Bulletin.
15(3), 47-55.
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Tang, D. M., Cizmas, P., & Dowell, E. H.
Experiments and analysis for a gust generator in a wind tunnel. Journal of Aircraft.
33(1), 139-148.
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Cizmas, P., Tang, D., & Dowell, E. H.
Flow about a slotted cylinder-airfoil combination in a wind tunnel. Journal of Aircraft.
33(4), 716-721.
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Dorney, D. J., Sondak, D. L., Cizmas, P., Saren, V. E., & Savin, N. M.
Full-Annulus Simulations of Airfoil Clocking in A Compressor At Off-Design Operating Conditions. International Journal of Turbo and Jet Engines.
17(2), 95-117.
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Dorney, D. J., Sondak, D. L., Cizmas, P., Saren, V. E., & Savin, N. M.
Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor. International Journal of Turbo and Jet Engines.
16(3), 149-160.
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Cizmas, P., Hoenninger, C. R., Chen, S., & Martin, H. F.
Influence of Inter-row Gap Value on Turbine Losses. International Journal of Rotating Machinery.
7(5), 335-349.
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Slattery, J. C., & Cizmas, P.
Macro-scale fatigue fracture analysis of multiphase bodies, aircraft design, and catastrophic failure: Two aircraft accidents. Engineering Fracture Mechanics.
199, 274-279.
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Slattery, J. C., & Cizmas, P.
Macro-scale fracture analysis of isothermal composites: Theory and seven applications. Engineering Fracture Mechanics.
163, 366-380.
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Brown, R. L., Das, K., Cizmas, P., & Whitcomb, J. D.
Numerical Investigation of Actively Cooled Structures in Hypersonic Flow. Journal of Aircraft.
51(5), 1522-1531.
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Isvoranu, D. D., & Cizmas, P.
Numerical Simulation of Combustion and Rotor-Stator Interaction in a Turbine Combustor. International Journal of Rotating Machinery.
9(5), 363-374.
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Isvoranu, D. D., & Cizmas, P.
Numerical Simulation of Combustion and Rotor-Stator Interaction in a Turbine Combustor. International Journal of Rotating Machinery.
9(5), 363-374.
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Kirk, A. M., Gargoloff, J. I., Rediniotis, O. K., & Cizmas, P.
Numerical and experimental investigation of a serpentine inlet duct. International Journal of Computational Fluid Dynamics.
23(3), 245-258.
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Cizmas, P., & Dorney, D. J.
Parallel Computation of Turbine Blade Clocking. International Journal of Turbo and Jet Engines.
16(1), 49-60.
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Liliedahl, D. N., Carpenter, F. L., & Cizmas, P.
Prediction of Aeroacoustic Resonance in Cavities of Hole-Pattern Stator Seals. Journal of Engineering for Gas Turbines and Power.
133(2), 022504.
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Liliedahl, D. N., Carpenter, F. L., & Cizmas, P.
Prediction of Aeroacoustic Resonance in Cavities of Hole-Pattern Stator Seals. Mechanical Engineering.
134(04), 49-50.
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Liliedahl, D. N., Carpenter, F. L., & Cizmas, P.
Prediction of aeroacoustic resonance in cavities of hole-pattern stator seals. Mechanical Engineering.
134(4), 49-50.
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Krath, E. H., Carpenter, F. L., & Cizmas, P.
Prediction of unsteady flows in turbomachinery cascades using proper orthogonal decomposition. Physics of Fluids.
36(3),
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Cizmas, P., & Palacios, A.
Proper Orthogonal Decomposition of Turbine Rotor-Stator Interaction. Journal of Propulsion and Power.
19(2), 268-281.
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Cizmas, P. G., Palacios, A., O'Brien, T., & Syamlal, M.
Proper-orthogonal decomposition of spatio-temporal patterns in fluidized beds. Chemical Engineering Science (CES).
58(19), 4417-4427.
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Florea, R., Hall, K. C., & Cizmas, P.
Reduced-Order Modeling of Unsteady Viscous Flow in a Compressor Cascade. AIAA Journal.
36(6), 1039-1048.
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Florea, R., Hall, K. C., & Cizmas, P.
Reduced-order modeling of unsteady viscous flow in a compressor cascade. AIAA Journal.
36, 1039-1048.
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Slattery, J. C., Cizmas, P., Karpetis, A. N., & Chambers, S. B.
Role of differential entropy inequality in chemically reacting flows. Chemical Engineering Science (CES).
66(21), 5236-5243.
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Polewski, M. D., & Cizmas, P.
Several Cases for the Validation of Turbulence Models Implementation. Applied Sciences (Switzerland).
11(8), 3377-3377.
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Collard, J. E., & Cizmas, P.
The Effects of Vibrating Blades on Turbomachinery Rotor-Stator Interaction. International Journal of Turbo and Jet Engines.
20(1), 17-40.
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Cizmas, P., & Dorney, D. J.
The Influence of Clocking on Unsteady Forces of Compressor and Turbine Blades. International Journal of Turbo and Jet Engines.
17(2), 133-142.
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Chambers, S., Flitan, H., Cizmas, P., Bachovchin, D., Lippert, T., & Little, D.
The Influence of In Situ Reheat on Turbine-Combustor Performance. Journal of Engineering for Gas Turbines and Power.
128(3), 560-572.
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Freno, B. A., Matula, N. R., Fontenot, R. L., & Cizmas, P.
The use of dynamic basis functions in proper orthogonal decomposition. Journal of Fluids and Structures.
54, 332-360.
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Kim, K., & Cizmas, P.
Three-Dimensional Hybrid Mesh Generation for Turbomachinery Airfoils. Journal of Propulsion and Power.
18(3), 536-543.
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Hubbard, S. A., Fontenot, R. L., McFarland, D. M., Cizma, P., Bergman, L. A., Strganac, T. W., & Vakakis, A. F.
Transonic Aeroelastic Instability Suppression for a Swept Wing by Targeted Energy Transfer. Journal of Aircraft.
51(5), 1467-1482.
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Carpenter, F. L., Kassing, J., & Cizmas, P.
UNS3D Near-Field Predictions for the Third AIAA Sonic Boom Prediction Workshop. Journal of Aircraft.
59(3), 595-611.
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Freno, B. A., Brenner, T. A., & Cizmas, P.
Using proper orthogonal decomposition to model off-reference flow conditions. International Journal of Non-Linear Mechanics.
54, 76-84.
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Han, Z., & Cizmas, P.
A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors. International Journal of Turbo and Jet Engines.
20(1), 1-16.
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book
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Cizmas, P.
Aerothermodynamics and Jet Propulsion. Cambridge University Press (CUP).
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Cizmas, P.
Aerothermodynamics and Jet Propulsion. Cambridge University Press (CUP).
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chapter
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Flitan, H. C., Cizmas, P., Lippert, T., Bachovchin, D., & Little, D.
ANALYSIS OF UNSTEADY AEROTHERMODYNAMIC EFFECTS IN A TURBINE-COMBUSTOR. UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES.
(pp. 551-566).
Springer Nature.
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Florea, R., Hall, K. C., & Cizmas, P.
Eigenmode Analysis of Unsteady Viscous Flows in Turbomachinery Cascades. Unsteady Aerodynamics and Aeroelasticity of Turbomachines.
(pp. 767-782).
Springer Nature.
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Cizmas, P., & Subramanya, R.
Parallel Computation of Rotor-Stator Interaction. Unsteady Aerodynamics and Aeroelasticity of Turbomachines.
(pp. 633-645).
Springer Nature.
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Isvoranu, D., Danaila, S., Cizmas, P., & Leventiu, C.
Proper Orthogonal Decomposition Applied to a Turbine Stage with In-Situ Combustion. Advances in Energy Research.
3rd International Congress on Energy Efficiency and Energy Related Materials (ENEFM2015).
(pp. 11-17).
Springer Nature.
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Flitan, H. C., Cizmas, P., Lippert, T., Bachovchin, D., & Little, D.
ANALYSIS OF UNSTEADY AEROTHERMODYNAMIC EFFECTS IN A TURBINE-COMBUSTOR. UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES.
(pp. 551-566).
Springer Nature.
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conference paper
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Han, Z., & Cizmas, P.
A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors. v001t03a086-v001t03a086.
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Strganac, T., & Cizmas, P.
A Comprehensive Approach to Simulate Nonlinear Aeroelastic Response
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Carpenter, F. L., Cizmas, P., Bolander, C. R., Giblette, T. N., & Hunsaker, D. F.
A Multi-Fidelity Optimization Study Investigating Distributed Adaptivity for Robust Low-Boom Performance
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Cizmas, P. G., & Schoppe, J.
A Multi-Limiter Method for Simulating Complex Flows on Large Grids
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Blanchard, A., Schoppe, J., Reddy, S., Dulikravich, G. S., & Cizmas, P. G.
A Multi-Objective Hybrid Optimization Methodology for Minimizing Aircraft Sonic Boom and Drag at Fixed Lift
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Gargoloff, J., Cizmas, P., Strganac, T., & Beran, P.
A Parallel Multigrid Algorithm for Aeroelasticity Simulations. 4041-4058.
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Krath, E. H., Carpenter, F. L., & Cizmas, P.
A Proper Orthogonal Decomposition Method for Analysis of Unsteady Flows in Turbomachinery Cascades. 1-18.
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Freno, B., & Cizmas, P.
A Proper Orthogonal Decomposition Method for Nonlinear Flows with Deforming Meshes
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Brenner, T. A., Carpenter, F. L., Freno, B. A., & Cizmas, P.
A REDUCED-ORDER MODEL FOR TURBOMACHINERY FLOWS USING PROPER ORTHOGONAL DECOMPOSITION. v06bt37a020-v06bt37a020.
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Cizmas, P., & Hall, K. C.
A viscous-inviscid model of unsteady small-disturbance flows in cascades
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Reddy, S. R., Dulikravich, G. S., Carpenter, F. L., & Cizmas, P.
Achieving Quieter Supersonic Flight Through Outer-Mold Line Modifications: An Optimization Study
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Strganac, T., Cizmas, P., Nichkawde, C., Gargoloff, J., & Beran, P.
Aeroelastic Analysis for Future Air Vehicle Concepts Using a Fully Nonlinear Methodology. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
4575-4608.
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McFarland, D., Cizmas, P., Strganac, T., Bergman, L., Lee, Y., Vakakis, A., & Hubbard, S.
Aeroelastic Analysis of a Transonic Wing for Design of Local Nonlinear Attachments. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
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Brown, R., Das, K., Whitcomb, J., & Cizmas, P.
Aeroelastic Simulation of Structures in Hypersonic Flow. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
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Brown, R. L., Das, K., Whitcomb, J. D., & Cizmas, P.
Aeroelastic simulation of structures in hypersonic flow
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Cizmas, P.
An Acceleration Approach for Reduced-Order Models Based on Proper Orthogonal Decomposition. 8825-8834.
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Krath, E., Carpenter, F. L., & Cizmas, P.
Analysis of Turbine Viscous Flow using a Novel Proper Orthogonal Decomposition Method
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Collard, J., & Cizmas, P.
Blade-forced vibration effects on turbomachinery rotor-stator interaction
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Weaver-Rosen, J. M., Carpenter, F. L., Cizmas, P. G., Malak, R. J., Abraham, T. A., Hunsaker, D. F., & Lazzara, D. S.
Computational Design Methodology of Adaptive Outer Mold Line for Robust Low En-Route Noise of a Supersonic Aircraft
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Carpenter, F. L., Cizmas, P. G., Reddy, S. R., & Dulikravich, G. S.
Controlling Sonic Boom Loudness Through Outer Mold Line Modification: A Sensitivity Study
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Jones, N. H., Cizmas, P., & Slattery, J. C.
Creating Reduced Kinetics Models That Satisfy the Entropy Inequality. v04at04a047-v04at04a047.
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Carpenter, F. L., & Cizmas, P. G.
Effect of Gradient Reconstruction Method on Transonic Fan Performance
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Dorney, D. J., Sondak, D. L., & Cizmas, P. G.
Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine. International Journal of Turbo and Jet Engines.
119-132.
-
Dorney, D., Sondak, D., & Cizmas, P.
Effects of hot streak/airfoil ratio in a high-subsonic single-stage turbine
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Dorney, D. J., Sondak, D. L., Cizmas, P., Saren, V. E., & Savin, N. M.
Full-Annulus Simulations of Airfoil Clocking in A Compressor At Off-Design Operating Conditions. International Journal of Turbo and Jet Engines.
95-118.
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Dorney, D. J., Sondak, D. L., Cizmas, P., Saren, V. E., & Savin, N. M.
Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor. v001t03a002-v001t03a002.
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Dorney, D., Sondak, D., Cizmas, P., Saren, V., & Savin, N.
Full-annulus simulations of airfoil clocking in a compressor at off-design operating conditions
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Carpenter, F., Johnson, S., Cizmas, P., & Rediniotis, O.
Internal Plenum Design and Testing for an Oscillatory Blowing Rotating Stall Suppression System
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Mitran, S., & Cizmas, P.
LES calibration of a turbulent potential model for turbomachinery flows
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Mitran, S. M., & Cizmas, P. G.
LES calibration of a turbulent potential model for turbomachinery flows
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Mitran, S. M., & Cizmas, P. G.
LES calibration of a turbulent potential model for turbomachinery flows
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Gargoloff, J., & Cizmas, P.
Mesh Generation and Deformation Algorithm for Aeroelasticity Simulations. 6716-6731.
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Cizmas, P., & Gargoloff, J. I.
Mesh Generation and Deformation Algorithm for Aeroelasticity Simulations. Journal of Aircraft.
1062-1066.
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Standridge, J., Comsa, C., Pannkuk, T., & Cizmas, P.
NUMERICAL SIMULATION OF UNSTEADY FLOWS IN LABYRINTH SEALS. 1-12.
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Matula, N. R., & Cizmas, P. G.
Numerical Investigation of the Effect of Geometric Design Parameters on Swirl Brake Performance
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Kirk, A., Kumar, A., Gargoloff, J., Rediniotis, O., & Cizmas, P.
Numerical and Experimental Investigation of a Serpentine Inlet Duct. 10240-10253.
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Liliedahl, D. N., Carpenter, F. L., & Cizmas, P.
PREDICTION OF AEROACOUSTIC RESONANCE IN CAVITIES OF HOLE-PATTERN STATOR SEALS. 349-361.
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Gargoloff, J., Cizmas, P., Strganac, T., & Beran, P.
Parallel Algorithm for Fully Nonlinear Aeroelastic Analysis. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
5772-5782.
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Cizmas, P., Gargoloff, J. I., Strganac, T. W., & Beran, P. S.
Parallel Multigrid Algorithm for Aeroelasticity Simulations. Journal of Aircraft.
53-63.
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Cizmas, P., & Dorney, D.
Parallel computation of turbine blade clocking
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Brenner, T., Cizmas, P., O'Brien, T., & Breault, R.
Practical Aspects of the Implementation of Proper Orthogonal Decomposition
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Liliedahl, D., & Cizmas, P.
Prediction of Fluid Instabilities in Hole-Pattern Stator Seals
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Freno, B., Brenner, T., & Cizmas, P.
Proper Orthogonal Decomposition Applied to the Reynolds-Averaged Navier--Stokes Equations
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Krath, E. H., Carpenter, F. L., Cizmas, P., & Johnston, D. A.
REDUCED-ORDER MODEL OF UNSTEADY FLOWS IN A TURBOMACHINERY FAN MODELED USING A NOVEL PROPER ORTHOGONAL DECOMPOSITION
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Florea, R., Hall, K., & Cizmas, P.
Reduced order modelling of unsteady viscous flow in a compressor cascade
-
Florea, R., Hall, K. C., & Cizmas, P.
Reduced-Order Modeling of Unsteady Viscous Flow in a Compressor Cascade. AIAA Journal.
1039-1048.
-
Cizmas, P.
Simultaneous method for calculating interacting boundary layers using a solid body mode. 1-11.
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Carpenter, F., Johnson, S., Cizmas, P., & Rediniotis, O.
Single-Stage Axial Compressor for the Study of Rotating Stall Suppression
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Hubbard, S., McFarland, M., Vakakis, A., Bergman, L., Fontenot, R., Brown, R., Cizmas, P., & Strganac, T.
Stability Enhancement of a Transonic Wing Using a Simple Passive Attachment
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Weaver-Rosen, J., Tsai, Y., Schoppe, J., Terada, Y., Malak, R., Cizmas, P. G., & Lazzara, D. S.
Surrogate Modeling and Parametric Optimization Strategy for Minimizing Sonic Boom in a Morphing Aircraft
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Carpenter, F. L., & Cizmas, P.
TRANSONIC FAN PERFORMANCE EVALUATED WITH DIFFERENT SOLUTION LIMITERS. v02bt41a054-v02bt41a054.
-
Chambers, S., Flitan, H., Cizmas, P., Bachovchin, D., Lippert, T., & Little, D.
The Influence of In Situ Reheat on Turbine-Combustor Performance. 601-612.
-
Freno, B., Brown, R., & Cizmas, P.
The Role of Structural Nonlinearities in Wind Turbine Blade Aeroelastic Analysis
-
Freno, B. A., Fontenot, R., Matula, N., & Cizmas, P. G.
The Use of Dynamic Basis Functions in Proper Orthogonal Decomposition
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Blumenfeld, M., & Cizmas, P.
The accurate element method: A novel method for integrating ordinary differential equations. Advances in the Astronautical Sciences.
446-461.
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Blumenfeld, M., & Cizmas, P.
The accurate element method: A novel method for integrating ordinary differential equations. Advances in the Astronautical Sciences.
445-459.
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Freno, B. A., Matula, N. R., Fontenot, R. L., & Cizmas, P.
The use of dynamic basis functions in proper orthogonal decomposition. Journal of Fluids and Structures.
332-360.
-
Kim, K., & Cizmas, P.
Three-Dimensional Hybrid Mesh Generation for Turbomachinery Airfoils. Journal of Propulsion and Power.
536-543.
-
Kassing, J., Carpenter, F. L., & Cizmas, P.
UNS3D Simulations for the Third Sonic Boom Prediction Workshop Part I: Biconvex 97 Shock-Plume Interaction Model
-
Carpenter, F. L., & Cizmas, P.
UNS3D Simulations for the Third Sonic Boom Prediction Workshop Part II: C608 Low-Boom Flight Demonstrator
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Han, Z., & Cizmas, P.
A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors. v001t03a086-v001t03a086.
-
institutional repository document
-
Krath, E. H., Carpenter, F. L., Cizmas, P., & Johnston, D. A.
An Efficient Proper Orthogonal Decomposition based Reduced-Order Model
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Krath, E. H., Carpenter, F. L., Cizmas, P., & Johnston, D. A.
An Efficient Proper Orthogonal Decomposition based Reduced-Order Model
Research
principal investigator on
- The Role of Second Law of Thermodynamics in Deriving Turbulence Models and Simplified Reaction Kinetics awarded by Los Alamos National Laboratory - (Los Alamos, New Mexico, United States) 2022 - 2025
- A Two-Phase Flow CFD Model for Predicting Rotordynamic Performance of Annular Seals During Laminar-to-Turbulent Transition awarded by Turbomeca - (Bordes, France) 2021 - 2023
- A Two-Phase Flow CFD Model for Predicting Rotordynamic Performance of Annular Seals During Laminar-to-Turbulent Transition awarded by Turbomeca - (Bordes, France) 2021 - 2023
- A Two-Phase Flow CFD Model for Predicting Rotordynamic Performance of Annular Seals During Laminar-to-Turbulent Transition (Cizmas, Paul) awarded by Turbomachinery Research Consortium - (College Station, Texas, United States) 2021 - 2023
- A Two-Phase Flow CFD Model for Predicting Rotordynamic Performance of Annular Seals During Laminar-to-Turbulent Transition (Cizmas, Paul) awarded by Turbomachinery Research Consortium - (College Station, Texas, United States) 2021 - 2023
- An Experimental and Computational Investigation of the Rotordynamic Coefficients of a Labyrinth Seal awarded by Turbomeca - (Bordes, France) 2018 - 2023
- An Experimental and Computational Investigation of the Rotordynamic Coefficients of a Labyrinth Seal awarded by Turbomeca - (Bordes, France) 2018 - 2023
- An Experimental and Computational Investigation of the Rotordynamic Coefficients of a Labyrinth Seal (Cizmas, Paul) awarded by Turbomachinery Research Consortium - (College Station, Texas, United States) 2018 - 2023
- An Experimental and Computational Investigation of the Rotordynamic Coefficients of a Labyrinth Seal (Cizmas, Paul) awarded by Turbomachinery Research Consortium - (College Station, Texas, United States) 2018 - 2023
- A ζ-coordinate Proper Orthogonal Decomposition Method with Dynamic Basis Functions for Turbomachinery Aeroelastic Analysis awarded by Ohio Aerospace Institute - (Cleveland, Ohio, United States) 2015 - 2019
- A ζ-coordinate Proper Orthogonal Decomposition Method with Dynamic Basis Functions for Turbomachinery Aeroelastic Analysis awarded by Ohio Aerospace Institute - (Cleveland, Ohio, United States) 2015 - 2019
- Study of the Effect of Methane Ingestion on Turboshaft Engine Performance awarded by American Bureau of Shipping - (Houston, Texas, United States) 2015
co-principal investigator on
- Supersonic Flight Test Design Study and Planning for Adaptive Geometries and LIDAR awarded by National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States) 2023 - 2025
- D.5 University Leadership Initiative awarded by National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States) 2017 - 2022
- Development of Reduced Order Models for Reacting Gas-Solid Flow using Proper Orthogonal Decomposition awarded by National Energy Technology Laboratory - (South Park Township, Pennsylvania, United States) 2014 - 2017
- (MURI 09) Synthesis, Characterization and Modeling of Functionally Graded Multifunctional Hybrid Composites for Extreme Environments awarded by United States Air Force - (Arlington, Virginia, United States) 2009 - 2015
Teaching
teaching activities
- AERO351 Aerothermo Propulsion Instructor
- AERO415 Comp Fluid Dyn Aero Apps Instructor
- AERO417 Aerospace Propulsion Instructor
- AERO452 Heat Trans Visc Flows Instructor
- AERO489 Sptp: Comp Fluid Dyn For Aero Instructor
- AERO489 Sptp:comp Flu Dyn For Aero App Instructor
- AERO491 Hnr-research Instructor
- AERO491 Hnr-research Instructor
- AERO615 Comp Fluid Dynamics Aero Appl Instructor
- AERO684 Professional Internship Instructor
- AERO685 Directed Studies Instructor
- AERO691 Research Instructor
- AERO691 Research Instructor
Works By Students
chaired theses and dissertations
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Brenner, Thomas Andrew (2012-07). Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition.
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Brown II, Robert Lee (2016-07). Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.
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Carpenter IV, Forrest Lafon (2016-07). Practical Aspects of Computational Fluid Dynamics for Turbomachinery.
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Carter, Jerry W. (2011-08). Implementation of a Lower-Upper Symmetric Gauss-Seidel Implicit Scheme for a Navier-Stokes Flow Solver.
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Chambers, Steven B. (2005-02). Investigation of combustive flows and dynamic meshing in computational fluid dynamics.
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Fontenot, Raymond Lee (2012-02). Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows.
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Freno, Brian Andrew (2011-08). An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.
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Freno, Brian Andrew (2013-11). Reduced-order Models for Computational Aeroelasticity.
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Gargoloff, Joaquin Ivan (2009-05). A numerical method for fully nonlinear aeroelastic analysis.
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Guarnieri, Jason Antonio (2005-02). Thermal signature reduction through liquid nitrogen and water injection.
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Joly, Michael Marie (2014-07). Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.
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Jones, Nathan (2012-10). The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms.
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Kim, Kyusup (2005-02). Three-dimensional hybrid grid generator and unstructured flow solver for compressors and turbines.
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Liliedahl, David Noel (2017-06). A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis.
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Ream, Allen (2015-08). Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality.
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Resendiz Rosas, Celerino (2005-08). Numerical simulation of flow separation control by oscillatory fluid injection.
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Richardson, Brian Ross (2009-05). A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows.
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Worley, Gregory (2010-07). A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations.
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Yuan, Tao (2005-02). Reduced order modeling for transport phenomena based on proper orthogonal decomposition.
Background
education and training
awards and honors
- Research and Technology Performance and Innovation Award, conferred by Boeing - (Chicago, Illinois, United States), 2018
- Fellow, conferred by American Society of Mechanical Engineers - (New York, New York, United States), 2016
- Herbert H. Richardson Faculty Fellow, conferred by Texas A&M University - (College Station, Texas, United States), 2009
- E.D. Brockett Professorship, conferred by Texas A&M University - (College Station, Texas, United States), 2008
- Associate Fellow, conferred by American Institute of Aeronautics and Astronautics - (Reston, Virginia, United States), 2002
- Technical Publication Award, conferred by Westinghouse Science and Technology - (United States), 1997
Contact
first name
- Paul
has last name
- Cizmas
mailing address
-
Texas A&M University
Aerospace Engineering
3141 TAMU
College Station, TX 77843-3141
USA
Other
- cizmas@tamu.edu