Assessment of thermochemical nonequilibrium and slip effects for orbital keentry experiment (OREX) by

31st Thermophysics Conference

Volumn , Issue , 1996, Pages

  Gupta, Roop N ^a   Moss, James N ^a   Price, Joseph M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL ANALYSIS; FORECASTING; HEAT TRANSFER; MONTE CARLO METHODS;

ALTITUDE RANGE; CHEMICAL MODEL; DATA EXTRACTION; DIRECT SIMULATION MONTE CARLO; ELECTRON NUMBER DENSITIES; LOW DENSITY EFFECTS; ORBITAL RE-ENTRY EXPERIMENTS; THERMOCHEMICAL NONEQUILIBRIUM;

FLOW FIELDS;

EID: 84964462229     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

1. Gupta, R. N., “Viscous Shock-Layer Study of Thermochemical Nonequihbrium,” Journal of Thermophvsics and Heat Transfer. Vol. 10, No. 2,1996, pp. 257-266.
2. Inouye, Y., “OREX Flight-Quick Report and Lessons Learned,” Invited paper 4, 2nd European Symposium on Aerothermodynamics of Space Vehicles, ESTEC, Nov. 1994.
3. Yamamoto, Y. and Yoshioka, M., “CFD and FEM CoupKng Analysis of OREX Aerothermodynamic Flight Data,” AIAA Paper 95-2087, June 1995.
4. Moss, J. N. and Bird, G. A, “Direct Simulation Transitional Flow for Hypersonic Re-entry Conditions,” Progress in Astronautics and Aeronautics: Thermal Design of Aeroassisted Orbital Vehicles, edited by H. F. Nelson, Vol. 96, 1985, pp. 113-139.
5. Yamamoto, Y., private communication, Aerodynamics Division, National Aerospace Lab., Tokyo-182, Japan, Dec. 1995.
6. Watanabe, Y., Inouye, Y., Wada Y., Akimoto, T., and Fujiwara, T., “Computational and Experimental Studies on an Electrostatic Probe and Catalytic Effect Sensor for a Reentry Experiment,” AIAA Paper 93-0479, Jan. 1993.
7. Bird, G. A., “Molecular Gas Dynamics and the Direct Simulation of Gas Flows.” Clarendon Press, Oxford, 1994.
8. NAL/NASDA Joint Research Report. OREX, March 1995 (in Japanese).
9. Jones, W. L., Jr., and Cross, A. E., “Electrostatic Probe Measurements of Plasma Parameters for Two Reentry Flight Experiments at 25000 Feet Per Second,” NASATN D-6617, April 1972.
10. Gupta, R. N. and Lee, K. P., “Thermo-chemical Nonequilibrium Analysis of Viscous Shock-Layers,” AIAA Paper 95-2083, June 1995.
11. Park, Chul, “Nonequilibrium Aerothermodvnamics.” Wiley, New York, 1990, pp. 103-115.
12. Gupta, R. N, “Réévaluation of Flight-Derived Surface Recombination-Rate Expressions for Oxygen and Nitrogen,” Journal of Spacecraft and Rockets. Vol. 34, No. 1, Jan. -Feb. 1997.
13. Moss, J. N. and Price, J. M., “DSMC Calculations for OREX Entry and Comparison with Flight Measurements in the Transitional Flow Regime,” To appear as NASA TM, 1996.
14. Anon., U.S. Standard Atmosphere. U.S. Government Printing Office, Washington, DC, Dec. 1962.
15. Jacchia, L. O, “Thermospheric Temperature, Density and Composition: New Modes,” Research in Space Science. Smithsonian Institution Astrophysical Observatory, SAO Special Report 375, Cambridge, MA, March 1977.
16. Celenligil, M. O, Moss, J. N., and Blanchard, R C, “Three-Dimensional Rarefied Flow Simulations for the Aeroassist Flight Experiment Vehicle,” AIM Journal, Vol. 29, No. 1, Jan. 1991, pp. 52-57.
17. Gupta, R. N., “Stagnation Flowfield Analysis for an Aeroassisted Vehicle,” Journal of Spacecraft and Rockets, Vol. 30, No. 1, Jan. -Feb. 1993, pp. 14-21.
18. US-European Conference on High Speed Flow Fields, Dept. of Mathematics, University of Houston, Texas, November 1995.
19. Throckmorton, D. A., “Benchmark Aeroheating Data From the First Flights of the Space Shuttle Orbiter,” AIAA Paper 82-0003, Jan. 1982.
20. Gupta, R. N. and Simmonds, A L., “Hypersonic Low-Density Solutions of the Navier-Stokes Equations with Chemical Nonequi H brium and Multicomponent Surface Slip,” AIAA Paper 86-1349, June 1986.
21. Moss, J. N.; Cuda, V., Jr.; and Simmonds, A L., “Nonequilibrium Effects for Hypersonic Transitional Flows,” AIAA Paper 87-0404, Jan. 1987.