Chemical non-equilibrium flow simulation of plasma wind tunnel test of HSP crew module

Author:

Ajith M.,Aravindakshan Pillai L.,Dileep K.N.,Sreenivas N.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference11 articles.

1. Hypersonic mach number and real gas effects on space shuttle orbiter aerodynamics;Maus;J. Spacecraft Rockets,1984

2. Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles;Hassan;J. Spacecraft Rockets,1993

3. Real-gas flowfields about three-dimensional configurations;Balakrishnan;J. Spacecraft Rockets,1985

4. Theory of stagnation point heat transfer in dissociated air;Fay;J. Aeronautical Sci.,1958

5. Hypersonic and High Temperature Gas Dynamics;Anderson,1989

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