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Hypersonic Aerothermodynamics: Past, Present and Future

  • Park, Chul (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology)
  • Received : 2013.02.14
  • Accepted : 2013.02.24
  • Published : 2013.03.30

Abstract

This is a written version of the keynote speech delivered at the International Symposium on Hypersonic Aerothermodynamics - Recent Advances held in Bangalore, India, from December $6^{th}$ to $10^{th}$, 2012. In this document, what was accomplished in the past, the present status, and what is expected in the future in the field of hypersonic aerothermodynamics are reviewed. Solved problems are categorized into four items; unsolved problems into twelve items, and emerging problems into four items. Removing one degree uncertainty in trim angle of attack, studying the thermochemical phenomena in a hydrogen-helium-methane mixture, and entry flights of meteoroids are cited as the tasks for the future.

Keywords

References

  1. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, John Wiley and Sons, New York, NY, 1990, pp.306-312.
  2. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, John Wiley and Sons, New York, NY, 1990, 312-316.
  3. Sharma, S. P. and Gillespie, W., "Nonequilibrium and Equilibrium Shock Front Radiation Measurements," Journal of Thermophysics and Heat Transfer, Vol. 5, No. 3, 1991, pp. 257-265. https://doi.org/10.2514/3.259
  4. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, John Wiley and Sons, New York, NY, 1990, p.281.
  5. Kim, J. G., and Boyd, I., "Master Equation Analysis of Thermochemical Nonequilibrium of Nitrogen," 43rd AIAA Thermophysics Conference, New Orleans AIAA Paper 2012-3305, 2012.
  6. Park, C., Nonequilibrium Hypersonic Aerothermodynamics, John Wiley and Sons, New York, NY, 1990, pp.89-92.
  7. Holden, M. S., Wadhams, T. P., MacLean, M., Dufrene, A., Mundy, E., and Marineau, E., "A Review of Basic Research and Development Programs Conducted in the LENS Facilities in Hypervelocity Flows," 50th AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, AIAA Paper 2012-169, 2012..
  8. Furudate, M., Nonaka, S., and Sawada, K., "Behavior of Two-Temperature Model in Intermediate Hypersonic Regime," Journal of Thermophysics and Heat Transfer, Vol. 13, No. 4, 1999, pp. 424-430. https://doi.org/10.2514/2.6480
  9. Fujita, K., Sato, 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. https://doi.org/10.2514/2.6654
  10. Dankert, C., "Rarefied Flow Investigation in Gas- Surface Interaction and Supersonic Plumes," Colloquium on Nonequilibrium Phenomena of Low-Density Jets in Space, Kyoto University, 1998, pp.51-60.
  11. Park, C., "Rotational Relaxation of $N_{2}$ Behind a Strong Shock Wave," Journal of Thermophysics and Heat Transfer, Vol. 18, No. 4, 2004, pp.527-533. https://doi.org/10.2514/1.11442
  12. Matsuyama, S., Ohnishi, N., Sasoh, A., and Sawada, K., "Numerical Simulation of Galileo Probe Entry Flowfield With Radiation and Ablation," Journal of Thermophysics and Heat Transfer, Vol. 19, No. 1, 2005, pp.28-35. https://doi.org/10.2514/1.10264
  13. Park, C., "Stagnation-Region Heating Environment of the Galileo Probe," Journal of Thermophysics and Heat Transfer, Vol. 23, No. 3, 2009, pp.417-424. https://doi.org/10.2514/1.38712
  14. Park, C., "Nonequilibrium Chemistry and Radia-tion for Neptune Entry," Journal of Spacecraft and Rockets, Vol. 48, No. 6, 2011, pp.897-903. https://doi.org/10.2514/1.51810
  15. Leibowitz, L. P., "Measurement of the Structure of an Ionizing Shock Wave in a Hydrogen-Helium Mixture," The Physics of Fluids, Vol. 16, No. 1, 1973, pp.59-68. https://doi.org/10.1063/1.1694174
  16. Livingston, F. R., and Poon, T. Y., "Relaxation Distance and Equilibrium Electron Density Measurements in Hydrogen-Helium Plasmas," AIAA Journal, Vol. 14, No. 9, 1976, pp.1335-1337. https://doi.org/10.2514/3.61466
  17. Bogdanoff, D. W., and Park, C., "Radiative Interaction Between Driver and Driven Gases in an Arc-Driven Shock Tube," Shock Waves, Vol. 12, No. 1, 2002, pp.205-214. https://doi.org/10.1007/s00193-002-0157-y
  18. Omura, M., and Presley, L. L., "Electron Density Measurements Ahead of Shock Waves in Air," AIAA Journal, Vol. 7, No. 12, 1969, pp.2363-2365. https://doi.org/10.2514/3.5554
  19. Park, C., Nonequilibrium Hypersonic Aer-othermodynamics, John Wiley and Sons, New York, NY, 1990, pp.303- 306.
  20. Wada, Y., Watanabe, Y., Akimoto, T., and Yasui, H. "Data Analysis of Electrostatic Probe," Proceedings of HOPE/ OREX Workshop (in Japanese), Tokyo, paper F-2, 1994.
  21. Park, C., "Injection-Induced Turbulence in Stagnation- Point Boundary Layers," AIAA Journal, Vol. 22, No. 2, 1984, pp.219-225. https://doi.org/10.2514/3.8371

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