Kinetic models analysis for super-orbital aerophysics

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Surzhikov, S T ^a   Shang, J S ^b  

^a INSTITUTE FOR PROBLEMS IN MECHANICS   (Russian Federation)

^b Wright State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONVECTIVE HEAT; DYNAMIC PROBLEM; FLIGHT EXPERIMENTS; GAS-PHASE REACTIONS; HYPERBOLIC VELOCITY; KINETIC MODELS; NON-EQUILIBRIUM RADIATION; RADIATION GAS; RADIATIVE HEATING; SPACE VEHICLES; TEMPERATURE FIELD;

AEROSPACE ENGINEERING; GAS DYNAMICS; KINETIC THEORY; THERMODYNAMICS; VEHICLES;

EARTH ATMOSPHERE;

EID: 78149442903     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Cornette, E.S., "Forebody Temperatures and Calorimeter Heating Rates Measured During Project Fire II Reentry at 11.35 km/s," NASA TM X-13 05, Nov. 1966.
2. Lewis J.H. and Scallion W.I., "Flight Parameters and Vehicle Performance for Project Fire Flight II, Launched May 22, 1965," NASA TN D-3565.
3. Cauchon, D.L., Mc Kee, C.W., and Cornette, E.S., "Spectral Measurements of Gas-Gap Radiation During FIRE Flight Experimentsat Reentry Velocities Near 11.4 kilometer per second," NASA TM X-1389.
4. Cauchon, D.L., "Radiative Heating Results From the FIRE II Flight Experiment at Reentry velocity of 11.4 km/s," NASA TM X-1402.
5. Surzhikov S.T., "Computing System for Solving Radiative Gasdynamic Problems of Entry and Re-Entry Space Vehicles," Proceedings of the International Workshop on Radiation of High Temperature Gases in Atmospheric Entry. 8-10 October 2003, Lisbon, Portugal. EAS SP-533, 2003, pp.111-117.
6. Olynick, D.R., Henline, W.D., Hartung L.C., and Candler, G.V., "Comparison of Coupled Radiative Navier-Stokes Flow Solutions with the Project Fire-II Flight Data," AIAA 94-1955, 1994, 15 p.
7. Tannehill, J.C., Anderson, D.A., Pletcher, R.H., Computational Fluid Mechanics and Heat Transfer. Second Edition, Taylor & Francis. 1997. p.792.
8. Gurvich, L.V., Veitc, I.V., Medvedev, V.A. et al., Thermodynamic Properties of Individual Substances. HandBook, Vols.1-4, Moscow: «Nauka», 1978.
9. http://webbook.nist.gov/chemistry.
10. Dunn, M.G. and Kang, S.W. "Theoretical and Experimental Studies of Reentry Plasmas," NASA CR 2232, April 1973.
11. Martin, J.J. Atmospheric Entry - An Introduction to its Science and Engineering. 1966, Old Tappan, NJ: Prentice-Hall (see also Bortner M.N. Chemical Kinetics in a Reentry Flow Field. R63SD63, King of Prussia, Pennsylvania, General Electric Space Science Laboratory, Missile and Space Division. 1963).
12. Park, C., "Review of Chemical-Kinetics Problems of Future NASA Missions, I: Earth Entries," Journal of Thermophysics and Heat Transfer, Vol.7, No.3, 1993.
13. Hirschfelder, J., Curtiss, C.F., and Bird, R.B., Molecular Theory of Gases and Liquids, Wiley, New York, 1966, p.562.
14. Gardiner, W.C.,Jr. (ed.) Combustion Chemistry, Springer-Verlag. 1984.
15. Bird, R.B., Stewart, W.E., Lightfoot, E.N., Transport Phenomena, 1965.
16. Capitelli M., Gorse C., Longo S., Giordano D., "Collision Integrals of High-Temperature Air Species," Journal of Thermophysics and Heat Transfer, 2000, Vol.14, No.2, P.259-268.