Heat transfer simulation and surface catalycity prediction at the Martian atmosphere entry conditions-Reference-Cited by-同舟云学术

Heat transfer simulation and surface catalycity prediction at the Martian atmosphere entry conditions

Published:1999-08-22 Issue: Volume: Page:
ISSN:
Container-title:9th International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Kolesnikov Anatoly¹,Yakushin Mikhail¹,Pershin Ivan¹,Vasil'evskii Sergey¹

Affiliation:

1. RAS, Inst. for Problems in Mechanics, Moscow, Russia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4892

Reference29 articles.

1. Kolesnikov A., Conditions of Simulation of StagnationPoint Heat Transfer from a High-Enthalpy Flow. Fluid Dynamics (tr. from . Russian),V. 28,N. 1,'1993,p. 131-137. " ~. !_.

2. Kolesnikov A.,The Aerothermodynamic Simulation in Sub- and .SupersonicHigh-EnthalpyJets:ExperimentandTheory.Proc.of ,the Second European Symposium on Aerothermodynamics'for Space Vehicles, ESTEC, Noordwijk,`The`Netherlands,21-25, November1994(ESA SP-367,February1995), p;583-590.

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