Analysis of hypersonic nonequilibrium flow over ablating surface

39th AIAA Fluid Dynamics Conference

Volumn , Issue , 2009, Pages

  Shang, J S ^a  

^a Wright State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL CHEMISTRY; KINETIC PARAMETERS; KINETIC THEORY;

ACCURACY IMPROVEMENT; AERODYNAMIC SIMULATIONS; CHEMICAL KINETIC MODEL; GOVERNING EQUATIONS; HIGH TEMPERATURE AIR; NON EQUILIBRIUM; NON-EQUILIBRIUM FLOWS; SPECIES CONCENTRATION;

BOUNDARY CONDITIONS;

EID: 78349272403     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-4051     Document Type: Conference Paper

References (32)

1. Milos, F. and Chen, Y., Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator, AIAA 2009-0262, Orlando FL, 2009.
2. Chen, Y.K., and Milos, F.S., Ablation and Thermal Response Program for Spacecraft Heatshield Analysis, J. Spacecraft and Rockets, Vol. 36, 1999, pp. 475-483.
3. Koo, J.H., Ho, D. and Ezekoye, O., A Review of Numerical and Experimental Characterization of Thermal Protection Materials - Part I., Numerical Modeling AIAA 2006-4936, July 2006.
4. Torre, L., Kenny, J.M., and Maffezzoli, Degradation Behavior of a Composite material for Thermal Protection System Part 1 - Experimental Characterization, J. of Material Science, Vol. 33, No.12, 1998, pp. 3137-3143. (Pubitemid 128509199)
5. Sutton, G., The Initial Development of Ablation Heat Protection, An Historical Perspective, J. Spacecraft & Rocket, Vol. 19, No. 1, 1982, pp. 3-11.
6. Park, C. and Balakrishnan, A., Ablation of Galileo Probe Heat-Shield Models in a Ballistic Range, AIAA J., Vol. 23, 1985, pp. 301-308.
7. Nachtsheim, P.R., and Larson, H.K., Crosshatched Ablation Patterns in Teflon, AIAA J., Vol. 9, No. 8. 1971, pp. 1608-1614.
8. Tobak, M., Hypothesis for the Origin of Cross-Hatching, AIAA J., Vol. 8, No. 2, 1970, pp. 330-334.
9. Chapman, S. and Cowling, T.G., The Mathematical theory of non-uniform Gases, Cambridge University Press, 1964, pp134-150.
10. Park, C., Stagnation-point Ablation of Carbonaceous Flat Disk, Part 1: Theory, AIAA J., Vol. 21, No. 11, 1983, pp. 1588-1594. (Pubitemid 14483733)
11. Zhluktov, S., and Abe, T, Viscous Shock-layer Simulation of Air flow past Ablating Blunt Body with Carbon Surface, Journal of Thermo-Physics and Heat Transfer, Vol. 13, No. 1, 1999, pp. 50-59.
12. Chen, Y.K. and Milo, F.S., Navier-Stokes Solutions with Finite Rate Ablation for Planetary Mission Earth Mission Earth Reentries, J. Spacecraft and Rockets, Vol. 42 No. 6, 2005, pp.961-970.
13. Park, C., Review of Chemical Kinetics Problems of Future NASA Missions, I Earth Entries, J. Thermophysics and Heat Transfer, Vol. 7 No. 3 1993.
14. Park, C., Chemical-kinetic Parameters of Hypersonic Earth Entry, J. of Thermophysics and heat Transfer, Vol. 15, No. 1, 2001, pp.76-90.
15. Lee, J.H., Basic Governing Equations for the Flight Regime of Aeroassisted Orbital Transfer Vehicles, Progress in Aeronautics and Astronautics: Thermal Design of Aeroassisted Orbital Transfer Vehicles, Vol. 96, AIAA, New York, NY, 1985, pp.3-53.
16. Candler, G.V., and MacCormack, R.W., Computation of Weakly ionized Hypersonic Flows in Thermochemical Nonequilibrium, J. Thermophysics, Vol. 5, No. 3, 1991, pp. 266-272.
17. Grasso, F. and Capano, G., Modeling of Ionizing Hypersonic Flows in Nonequilibrium, J. Spacecraft and Rockets, Vol. 32 1995, pp.217-224.
18. Josyula, E. and Bailey, W.F., Governing Equations for Weakly ionized Plasma Flow field of Aerospace Vehicles, J. Spacecraft and Rockets, Vol. 40, No. 6, 2003, pp. 845-857.
19. Surzhikov, S.T. and Shang, J.S., Kinetics Models Analysis for Super-Orbital Aerophysics, AIAA 2008-1278, Reno NV, 2008.
20. Shang, J.S., Surzhikov, S.T., Yan, H., Simulating Hypersonic Nonequilbrium Flow Using Kinetic Models, AIAA 2009-0286, Orland FL, 2009.
21. Clarke, J.F. and McChesney, M., The Dynamics of Real Gases, Butterworth Inc., Washington D.C., 1964, pp. 66-86.
22. Kraus, J.D., Electromagnetics, McGraw-Hill, New York, 1953, pp.445-480.
23. Jones, L.J. and Cross, A.E., Electrostatic Probe Measurements of Plasma Parameters for Two Reentry Flight Experiments at 25, 000 feet per second, NASA TN D 66-17, 1972.
24. Keenan, J.A., Candler, G.V., Simulation of Graphite Sublimation and Oxidation under Reentry Conditions, AIAA 94-2083, Colorado Springs CO, 1994.
25. Gosse, R., and Candler, G., Ablation Modeling of Electro-Magnetic Launched Projectile for Access to Space, AIAA 2007-1210, Reno NV, 2007.
26. Zel'dovich, Ya, B., and Raizer, Yu., P., Physics of Shock Waves and High-temperature Hydrodynamic Phenomena, Dover Publications, Mineola NY, 2002.
27. Landau, L. and Teller, E., Zur Theore der Schalldispersion, Physik Z. Sowjetunion, b. 10, h. 1, 1936, p.34.
28. Millikan, R.C., and White, D.R., Systematics of vibrational Relaxation, J. Chemical Physics, Vol. 39, No. 12, 1963, pp.3209-3213.
29. Treanor, C.E. and Marrone, P.V., Effect of Dissociation on the rate of Vibrational Relaxation, Physics of Fluids, Vol.5, No. 9., 1962, pp.1022-1026.
30. nd edition, John Wiley & Sons, New York, 2002, pp. 25, 274, 526.
31. Capitelli, M., Gorse, C., and Longo, S., J. Thermophysics and Heat Transfer, Vol. 14 No. 2, 2000, pp259-268.
32. Levin, E. and Wright, M.J., Collision Integrals for Ion-Neutral interactions of Nitrogen and Oxygen, J. Thermophysics and Heat Transfer, Vol.18 No 1, 2004, pp.143-147.