Viscous shock-layer study of thermochemical nonequilibrium

Journal of Thermophysics and Heat Transfer

Volumn 10, Issue 2, 1996, Pages 257-266

  Gupta, Roop N ^a,b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Gas Dynamics Division

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; AIR FLOW; RE-ENTRY FLIGHT;

CALCULATIONS; DENSITY (SPECIFIC GRAVITY); DESIGN; MATHEMATICAL MODELS; MIXTURES; MODELS; SENSITIVITY ANALYSIS; SURFACES; THERMODYNAMIC PROPERTIES; TRAJECTORIES; TRANSPORT PROPERTIES; VIBRATIONS (MECHANICAL);

AIRFLOW; CHEMICAL EQUILIBRIUM EFFECTS; ELECTRONIC NONEQUILIBRIUM; LOW DENSITY EFFECTS; MULTICOMPONENT MIXTURES; THERMOCHEMICAL NONEQUILIBRIUM; VISCOUS SHOCK LAYER TECHNIQUES;

VISCOUS FLOW;

EID: 0030111653     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/3.801     Document Type: Article

References (39)

1. Austin, R. E., and Cook, S. A., "SSTO Rockets: Streamlining Access to Space," Aerospace America, Vol. 32, Nov. 1994, pp. 34-39.
2. Weilmuenster, K. J., Gnoffo, P. A., Greene, F. A., Riley, C. J., Hamilton, H. H., II, and Alter, S. J., "Hypersonic Aerodynamic Characteristics of a Proposed Single-Stage-to-Orbit Vehicle," AIAA Paper 95-1850, June 1995.
3. Gnoffo, P. A., Gupta, R. N., and Shinn, J. L., "Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium," NASA TP 2867, Feb. 1989.
4. Palmer, G., "The Development of an Explicit Thermochemical Nonequilibrium Algorithm and Its Application to Compute Three Dimensional AFE Flowfields," AIAA Paper 89-1701, June 1989.
5. Candler, G. V., and MacCormack, R. W., "Computation of Weakly Ionized Hypersonic Flow in Thermo-Chemical Nonequilibrium," Journal of Thermophysics and Heat Transfer, Vol. 5, No. 3, 1991, pp. 266-273.
6. Walters, R. W., Cinnella, P., Slack, D. C., and Holt, D., "Characteristic-Based Algorithms for Flows in Thermochemical Nonequilibrium," AIAA Journal, Vol. 30, No. 5, 1992, pp. 1304-1313.
7. Greendyke, R. B., and Hartung, L. C., "A Convective and Radiative Heat Transfer Analysis for the Fire II Forebody," AIAA Paper 93-3194, July 1993.
8. Gally, T. A., and Carlson, L. A., "Survey of Nonequilibrium ReEntry Heating for Entry Flight Conditions," AIAA Paper 93-3230, July 1993.
9. Nishida, M., and Sakamura, Y., "Thermal and Chemical Nonequilibrium Viscous Shock Layer Flows over a Blunt Body at High Altitudes," Rarefied Gas Dynamics, edited by A. E. Beylich, Proceedings of the 17th International Symposium on Rarefied Gas Dynamics Aachen 1990, VCH Publishers, New York, 1991, pp. 514-521.
10. Suzuki, K., and Abe, T., "Viscous Shock-Layer Analysis of Thermally and Chemically Non-Equilibrium Forebody Flow of Mars Aerocapture Vehicle," AIAA Paper 93-2839, July 1993.
11. Gupta, R. N., Yos, J. M., Thompson, R. A., and Lee, K.-P., "A Review of Reaction Rates and Thermodynamic and Transport Properties for an 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30,000 K," NASA RP 1232, Aug. 1990.
12. Gupta, R. N., and Lee, K. P., "Thermo-Chemical Nonequilibrium Analysis of Viscous Shock-Layers," AIAA Paper 95-2083, June 1995.
13. Park, C., Nonequilibrium Aerothermodynamics, Wiley, New York, 1990, pp. 103-115.
14. Gupta, R. N., Lee, K.-P., and Zoby, E. V., "Enhancements to Viscous-Shock-Layer Technique," Journal of Spacecraft and Rockets, Vol. 30, No. 4, 1993, pp. 404-413.
15. Bird, R. B., Stewart, W. E., and Lightfoot, E. N., Transport Phenomena, Wiley, New York, 1960, pp. 563-572.
16. Park, C., "Assessment of Two-Temperature Kinetic Model for Ionizing Air," AIAA Paper 87-1574, June 1987.
17. Hansen, C. F., "Collision-Induced Gas Phase Dissociation Rates," Final Rept. on NASA Grant NAG1-1046, Aug. 1990.
18. Blottner, F. G., "Finite-Difference Methods of Solution of the Boundary-Layer Equations," AIAA Journal, Vol. 8, No. 2, 1970, pp. 193-206.
19. Lee, J. H., "Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles," edited by H. F. Nelson, Vol. 96, Progress in Aeronautics and Astronautics, AIAA, New York, 1985, pp. 3-53.
20. Lee, J. H., "Hypersonic Three-Dimensional Nonequilibrium Boundary-Layer Equations in Generalized Curvilinear Coordinates," NASA CR-185677, Feb. 1993.
21. Gupta, R. N., Scott, C. D., and Moss, J. N., "Slip-Boundary Equations for Multicomponent Nonequilibrium Airflow," NASA TP-2452, Nov. 1985.
22. Gupta, R. N., and Nayani, S. N., "Low-Density Flow Effects for Hyper-Velocity Vehicles," Air Force Flight Dynamics Lab., WRDC-TR-90-3007, Wright-Patterson AFB, OH, March 1990.
23. Gupta, R. N., Nayani, S. N., Lee, K. P., and Zoby, E. V., "Higher-Order Viscous Shock-Layer Solutions for High-Altitude Flows," Journal of Spacecraft and Rockets, Vol. 31, No. 5, 1994, pp. 751-758.
24. Lee, K. P., Gupta, R. N., Zoby, E. V., and Moss, J. N., "Hypersonic Viscous Shock-Layer Solutions over Long Slender Bodies - Part II: Low Reynolds Number Flows," Journal of Spacecraft and Rockets, Vol. 27, No. 2, 1990, pp. 185-193.
25. Lee, K. P., and Gupta, R. N., "Viscous-Shock-Layer Analysis of Hypersonic Flows," NASA CR-189614, March 1992.
26. Sakamura, Y., and Nishida, M., "Numerical Calculation of Thermal and Chemical Nonequilibrium Flows Around a Hypersonic Reentry Vehicle," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 34, No. 103, May 1991, pp. 27-45.
27. Akey, N. D., and Cross, A. E., "Radio Blackout Alleviation and Plasma Diagnostic Results from a 25,000 Foot Per Second Blunt-Body Reentry," NASA TN D-5615, Feb. 1970.
28. Granthan, W. L., "Flight Results of 25,000 Foot Per Second Reentry Experiment Using Microwave Reflectometers to Measure Plasma Electron Density and Standoff Distance," NASA TN D-6062, Dec. 1970.
29. Jones, W. L., Jr., and Cross, A. E., "Electrostatic Probe Measurements of Plasma Parameters for Two Reentry Flight Experiments at 25000 Feet Per Second," NASA TN D-6617, April 1972.
30. Gnoffo, P. A., "Code Calibration Program in Support of the Aeroassisted Flight Experiment," Journal of Spacecraft and Rockets, Vol. 27, No. 2, pp. 131-142.
31. Dunn, M. G., and Kang, S. W., "Theoretical and Experimental Studies of Re-entry Plasmas," NASA CR-2232, April 1993.
32. Cauchon, D. L., "Radiative Heating Results from the FIRE II Flight Experiment at a Reentry Velocity of 11.4 Kilometers Per Second," NASA TM X-1402, July 1967.
33. Gupta, R. N., "Navier-Stokes and Viscous Shock-Layer Solutions for Radiating Hypersonic Flows," AIAA Paper 87-1576, June 1987.
34. Zoby, E. V., and Sullivan, E. M., "Effects of Corner Radius on Stagnation-Point Velocity Gradients on Blunt, Axisymmetric Bodies," NASA TM X-1067, March 1965.
35. Hartung, L. C., "Development of a Nonequilibrium Radiative Heating Prediction Method for Coupled Flowfield Solutions," Journal of Thermophysics and Heat Transfer, Vol. 6, No. 4, 1992, pp. 618-625.
36. Zoby, E. V., "Approximate Heating Analysis for the Windward-Symmetry Plane of Shuttle-Like Bodies at Large Angle of Attack," AIAA Paper 81-1042, June 1981.
37. Zoby, E. V., Gupta, R. N., and Simmonds, A. L., Temperature-Dependent Reaction Rate Expressions for Oxygen Recombination, edited by H. F. Nelson, Vol. 96, Progress in Aeronautics and Astronautics, AIAA, New York, 1985, pp. 445-464.
38. Goldstein, H., "Reusable Thermal Protection System Development - A Perspective," NASA CP-3157, Feb. 1992.
39. Gupta, R. N., Lee, K. P., and Zoby, E. V., "Enhancements to Viscous-Shock-Layer Technique," Journal of Spacecraft and Rockets, Vol. 30, No. 4, 1993, pp. 404-413.