A comparison of EAST shock-tube radiation measurements with a new air radiation model

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Johnston, Christopher O ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATOMIC LINES; BOLTZMANN; COMPARISON WITH MEASUREMENTS; INITIAL PRESSURE; MOLECULAR BAND SYSTEMS; NON EQUILIBRIUM; NON-EQUILIBRIUM RADIATION; NONEQUILIBRIUM REGIMES; ORDER OF MAGNITUDE; PHYSICAL DATA; RADIATION MEASUREMENTS; RADIATION MODELS; RADIATIVE FLUXES; RATE MODELS; RETURN SHOCK; SHOCK VELOCITIES; SPECTRAL FEATURE; SPECTRAL RANGE; THERMOCHEMICAL NONEQUILIBRIUM; TUBE FLOW; WAVELENGTH RANGES;

AEROSPACE ENGINEERING; FORECASTING; SHOCK TUBES; UNCERTAINTY ANALYSIS;

RADIATION;

EID: 78149433943     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (40)

1. Johnston, C. O., Nonequilibrium Shock-Layer Radiative Heating for Earth and Titan Entry, Ph.D. Dissertation, Virginia Tech, November 2006.
2. Park, C., "Nonequilibrium Air Radiation (NEQAIR) Program: User's Manual," NASA TM 86707, 1985.
3. Nicolet, W.E., "Advanced Methods for Calculating Radiation Transport in Ablation-Product Contaminated Boundary Layers," NASA CR-1656, 1970.
4. Wilson, K.H., "RATRAP - A Radiation Transport Code," Lockheed Report 6-77-67-12, 1967.
5. Rigdon, W.S., Dirling, R.B., and Thomas, M., "Stagnation Point Heat Transfer During Hypervelocity Atmospheric Entry," NASA CR-1462, 1970.
6. 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.
7. Johnston, C.O., "Nonequilibrium Stagnation-Line Radiative Heating for Fire II," AIAA Paper 2007-3908, 2007.
8. Park, C., "Stagnation-Point Radiation for Apollo 4," Journal of Thermophysics and Heat Transfer, Vol. 18, 2004, pp. 349-357.
9. Gruszczynski, J.S., and Warren, W.R., "Study of Equilibrium Air Total Radiation," AIAA Journal, Vol. 5, No. 3, 1967, pp. 517-525.
10. Nerem, R.M., and Stickford, G.H., "Shock-Tube Studies of Equilibrium Air Radiation," AIAA Journal, Vol. 3, No. 6, 1965, pp. 1011-1018.
11. Thomas, G.M., and Menard, W.A., "Measurements of the Continuum and Atomic Line Radiation from High-Temperature Air, AIAA Journal, Vol. 5, No. 12, 1967, pp. 2214-2223.
12. Wood, A.D., Hoshizaki, H., Andrews, J.C., and Wilson, K.H., "Measurements of the Total Radiant Intensity of Air," AIAA Journal, Vol. 7, No. 1, 1969, pp. 130-138.
13. Sutton, K., "Air Radiation Revisited," AIAA Paper 84-1733, 1984.
14. Allen, R.A., Rose, P.H., and Camm, J.C., "Nonequilibrium and Equilibrium Radiation at Super-Satellite Re-Entry Velocities," AVCO Research Report 156, September 1962.
15. Sharma, S.P., "Nonequilibrium and Equilibrium Shock Front Radiation Measurements," Journal of Thermophysics and Heat Transfer, Vol. 5, No. 3, 1991, pp. 257-265.
16. Sharma, S.P., Assessment of Nonequilibrium Radiation Computation Methods for Hypersonic Flows," NASA TM-103994, 1993.
17. Sharma, S.P., and Whiting, E.E., "Modeling of Nonequilibrium Radiation Phenomena: An Assessment," Journal of Thermophysics and Heat Transfer, Vol. 10, No. 3, 1996, pp. 385-396.
18. Donohue, K., Reincecke, Rossi, D., Marinelli, W.J., Krech, R.H., and Caledonia, G.E., "Aerothermodynamic Radiation Studies," NASA CR-185666, 1991.
19. Koreeda, J., Ohama, Y., and Honma, H., "Imaging Spectroscopy of the Nonequilibrium Shock Front Radiation in Air," Shock Waves, Vol. 8, No. 2, 1998, pp. 71-78.
20. Morioka, T., Sakurai, N., Maeno, K., Honma, H., "Observation of Nonequilibrium Radiation behind Strong Shock Waves in Low-Density Air," Journal of Visualization, Vol. 3, No. 1, 2000, pp. 51-61.
21. Fujita, K., Sato, Sunichi, S., Abe, T., and Ebinuma, Y., "Experimental Investigation of Air Radiation from Behind a Strong Shock Wave," Journal of Thermophysics and Heat Transfer, Vol. 16, No. 1, 2002, pp. 77-82,.
22. Matsuda, A., Fujita, K., Sato, S., and Abe, T., "Nonequilibrium Phenomena Behind Strong Shock Waves Generated in Superorbital Reentry Flight," Journal of Thermophysics and Heat Transfer, Vol. 18, No. 3, 2004, pp. 342-348.
23. Grinstead, J., Wilder, M., Olejniczak, J., Bogdanoff, D., Allen, G., and Danf, K., "Shock-Heated Air Radiation Measurements at Lunar Return Conditions," AIAA Paper 2008-1244, 2008.
24. 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, 1989.
25. Park, C., "Review of Chemical-Kinetic Problems of Future NASA Missions, I: Earth Entries," Journal of Thermophysics and Heat Transfer, Vol. 7, pp. 385-398, 1993.
26. McBride, B.J., Zehe, M.J., and Gordon, S., "NASA Glenn Coefficients for Calculating Thermodynamic Properties of Individual Species," NASA TP 2002-211556, Sept. 2002.
27. Zeldovich, Y.B., and Raizer, Y.P., Physics of Shock Waves and High Temperature Hydrodynamic Phenomena, Vol. 1, Academic Press, New York and London, 1966.
28. Hartung, L.C., "Predicting Radiative Heat Transfer in Thermochemical Nonequilibrium Flow Fields," NASA TM-4564, 1994.
29. Wiese, W.L., Fuhr, J.R., and Deters, T.M., "Atomic Transition Probabilities of Carbon, Nitrogen, and Oxygen," Journal of Physical and Chemical Reference Data Monograph, No. 7, 1996.
30. Konjevic, N., and Roberts, J.R., "A Critical Review of Stark Widths and Shifts of Spectral Lines from Non-Hydrogenic Atoms," Journal of Physical and Chemical Reference Data, Vol. 5, No. 2, 1976, pp. 209-252.
31. Griem, H.R., Spectral Line Broadening by Plasmas, Academic Press, New York and London, 1974.
32. Whiting, E.E., "An Empirical Approximation to the Voigt Profile," Journal of Qualitative Spectroscopy and Radiative Transfer, Vol. 8, 1968, pp. 1379-1384.
33. Hartung, L.C., "Development of a Nonequilibrium Radiative Heating Prediction Method for Coupled Flowfield Solutions," Journal of Thermophysics and Heat Transfer, Vol. 6, 1992, pp. 618-625.
34. Laux, C.O., "Optical Diagnostics and Radiative Emission of Air Plasmas," High Temperature Gas Dynamics Lab, Mechanical Engineering Dept., Rept. T-288, Stanford University, 1993.
35. Johnston, C.O., Hollis, B.R., and Sutton, K., "Radiative Heating Methodology for the Huygens Probe," Journal of Spacecraft and Rockets, Vol. 44, No. 5, 2007, pp. 993-1002.
36. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1990.
37. Bultel, A., Cheron, B.G., Bourdon, A., Motapon, O., and Schneider, I.F., "Collisional-Radiative Model in Air for Earth Re-Entry Problems," Physics of Plasmas, Vol. 13, 2006, 043502.
38. Panesi, M., Magin, T.E., Bourdon, A., Bultel, A., Chazot, O., "Simulations of Nonequilibrium Reentry Air Plasmas by Means of a Collisional-Radiative Model," AIAA Paper 2007-4023, 2007.
39. Chauveau, S., Deron, C., Perrin, M.-Y., Riviere, P., Soufiani, A., "Radiative Transfer in LTE Air Plasmas for Temperatures up to 15, 00 K," Journal of Qualitative Spectroscopy and Radiative Transfer, Vol. 77, 2003, pp. 113-130.
40. Teulet, P., Sarrette, J.P., and Gomes, A.M., "Calculation of Electron Impact Inelastic Cross Sections and Rate Coefficients for Diatomic Molecules: Application to Air Molecules," Journal of Qualitative Spectroscopy and Radiative Transfer, Vol. 62, 1999, pp. 549-569.