Modeling of nonequilibrium radiation phenomena: An assessment

Journal of Thermophysics and Heat Transfer

Volumn 10, Issue 3, 1996, Pages 385-396

  Sharma, Surendra P ^a,c   Whiting, Ellis E ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b Thermosciences Institute   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

BAND STRUCTURE; COMPUTATIONAL METHODS; COMPUTER SOFTWARE; ELECTRON EMISSION; ELECTRON ENERGY LEVELS; ELECTRON TRANSITIONS; ELECTRONIC DENSITY OF STATES; HYPERSONIC AERODYNAMICS; PHASE EQUILIBRIA; QUANTUM ELECTRONICS; RADIATION; SHOCK WAVES;

CALCULATED SPECTRA; EINSTEIN TRANSITION PROBABILITY; ELECTRIC ARC DRIVEN SHOCK TUBE FACILITY; ELECTRON NUMBER DENSITY; ELECTRONIC STATES; EXCITATION RATE DATA; HYPERSONIC VEHICLES; NONEQUILIBRIUM RADIATION; PLANCK FUNCTION; VIBRATIONAL QUANTUM NUMBER;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0030197066     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/3.802     Document Type: Article

References (26)

1. Allen, R. A., Rose, P. H., and Camm, J. C., "Nonequilibrium and Equilibrium Radiation at Super-Satellite Re-Entry Velocities," AVCO Everett Research Lab., Research Rept. 156, Everett, MA, Sept. 1962.
2. Teare, J. D., Georgiev, S., and Allen, R. A., "Radiation from the Nonequilibrium Shock Front," AVCO Everett Research Lab., Research Rept. 112, Everett, MA, Oct. 1961.
3. Camm, J. C., Kivel, R. L., Taylor, R. L., and Teare, J. D., "Absolute Intensity of Nonequilibrium Radiation in Air and Stagnation Heating at High Altitudes," AVCO Everett Research Lab., Research Rept. 93, Everett, MA, Dec. 1959.
4. Sharma, S. P., and Gillespie, W. D., "Nonequilibrium and Equilibrium Shock Front Radiation Measurements," Journal of Thermophysics and Heat Transfer, Vol. 5, No. 3, 1991, pp. 257-265; also AIAA Paper 90-0139, Jan. 1990.
5. Sharma, S. P., Gillespie, W. D., and Meyer, S. A., "Shock Front Radiation Measurements in Air," AIAA Paper 91-0573, Jan. 1991.
6. Howe, J. T., "Introductory Aerothermodynamics of Advanced Space Transportation Systems," Journal of Spacecraft and Rockets, Vol. 22, No. 1, 1985, pp. 19-26.
7. Park, C., "Calculation of Nonequilibrium Radiation in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles," Thermal Design of Aeroassisted Orbital Transfer Vehicles, edited by H. F. Nelson, Vol. 96, Progress in Aeronautics and Astronautics, AIAA, New York, 1985, pp. 395-418.
8. Park, C., "Radiation Enhancement by Nonequilibrium in Earth's Atmosphere," Journal of Spacecraft and Rockets, Vol. 22, No. 1, 1985, pp. 27-36; also AIAA Paper 83-0410, Jan. 1983.
9. Page, W. A., and Arnold, J. O., "Shock Layer Radiation of Blunt Bodies at Entry Velocities," NASATR R-193, April 1964.
10. Seiff, A., Reese, D. E., Sommer, S. C., Kirk, D. B., Whiting, E. E., and Niemann H. B., "PAET, an Entry Probe Experiment in the Earth's Atmosphere," Icarus, International Journal of the Solar System, Vol. 18, No. 4, 1973, pp. 525-563.
11. Cauchon, D. L., "Project Fire Flight 1 Radiative Heating Experiment," NASA TM X-1222, April 1966.
12. Cauchon, D. L., "Radiative Heating Results from the Fire 2 Flight Experiment at a Reentry Velocity of 11.4 Kilometers per Second," NASA TM X-1402, July 1967.
13. Lee, D. B., and Goodrich, W. D., "The Aerothermodynamic Environment of the Apollo Command Module During Super-Orbital Entry," NASA TN D-6792, April 1972.
14. Curry, D. M., and Stephens, E. W., "Apollo Ablator Thermal Performance at Super-Orbital Entry Velocities," NASA TN D-5969, Sept. 1970.
15. Shirai, H., and Park, C., "Experimental Studies of Radiative Base Heating of a Jovian Entry Model," Entry Heating and Thermal Protection, edited by W. B. Olstad, Vol. 69, Progress in Astronautics and Aeronautics, AIAA, New York, 1980, pp. 148-171.
16. Park, C., "Calculation of Radiation from Argon Shock Layers," Journal of Quantitative Spectroscopy and Radiative Transfer, Vol. 28, No. 1, 1982, pp. 29-40.
17. Arnold, J. O., and Whiting, E. E., "Nonequilibrium Effects on Shock-Layer Radiometry During Earth Entry," Journal of Quantitative Spectroscopy and Radiative Transfer, Vol. 13, No. 9, 1973, pp. 861-870.
18. Cooper, D. M., Jaffe, R. L., and Arnold, J. O., "Computational Chemistry and Aeroassisted Orbital Transfer Vehicles," Journal of Spacecraft and Rockets, Vol. 22, No. 1, 1985, pp. 60-67.
19. Menees, G. P., "Thermal-Protection Requirements for Near-Earth Aeroassisted Orbital-Transfer Vehicle Missions," AIAA Paper 83-1513, June 1983.
20. Park, C., "Comparison of Electron and Electronic Temperatures in Recombining Nozzle Flow of Ionized Nitrogen-Hydrogen Mixture: Part 2 - Experiments," Journal of Plasma Physics, Vol. 9, Pt. 2, 1973, pp. 217-234.
21. Sharma, S. P., Huo, W. M., and Park, C., "The Rate Parameters for Coupled Vibration-Dissociation in a Generalized SSH Approximation," Journal of Thermophysics and Heat Transfer, Vol. 6, No. 1, 1992, pp. 9-21; also AIAA Paper 88-2714, June 1988.
22. Sharma, S., "Vibrational and Rotational Temperature Measurements in a Shock Tube," 18th International Symposium on Shock Waves, Sendai, Japan, July 1991.
23. Sharma, S. P., "Assessment of Nonequilibrium Radiation Computation Methods for Hypersonic Flows," International Journal of Modern Physics C, Vol. 4, No. 4, 1993, pp. 847-881; also NASA TM 103994, Jan. 1993.
24. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1990.
25. Whiting, E. E., and Park, C., "Radiative Heating at the Stagnation Point of the AFE Vehicle," NASA TM 102829. Nov. 1990.
26. Moreau, S., Laux, C. O., Chapman, D. R., and MacCormack, R. W., "A More Accurate Nonequilibrium Air Radiation Code: NEQAIR Second Generation," AIAA Paper 92-2968, July 1992.