Numerical Modeling of Hypersonic Aerodynamics and Heat Transfer Problems of the Martian Descent Modules

Author:

Shevelev Yuriy D.

Publisher

InTech

Reference43 articles.

1. Kay RD, Netterfield MP. Thermochemical Non-Equilibrium Computation For A Mars Entry Vehicle. AIAA Paper. No 93-2841; 1993

2. Gupta RN, Lee KP. An Aerothermal Study of MESUR Pathfinder Aeroshell. AIAA Paper. No 94-2025; 1994

3. Gallis MA, Harvey JK. Analysis of Non-Equilibrium in Mars Atmosphere Entry Flows. AIAA Paper. No 95-2095; 1995

4. Problems of Aerothermoballistics, Radiation Gasdynamics, Heat and Mass Transfer for Planet Sample Return Missions. Project Technical Report of ISTC No 1549-00; 2003. http://jan.imec.msu.ru/~avogadro/Mars/Mars1549/index.htm

5. Rouzaud O, Zhlukhtov S, Egorov I, Fletcher D, Gromov V, Nagnibeda E, Shevelev Yu, Omaly P. Numerical, analytical and experimental investigation of convective and radiative heating of a martian descent module. European Space Agency, ESA SP (583); 2005. pp. 93-98

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