Aerothermodynamic aspects of entry probe heat shield design

DOI10.1023/A:1001874903881zbMATH Open0945.76039MaRDI QIDQ1307882

V. Pereyra

Publication date: 12 October 2000

Published in: Astrophysics and Space Science (Search for Journal in Brave)

zbMATH Keywords

convective heat fluxradiative heat fluxaerothermal analysis of engineering problemsgas-material interfaceMars-entry vehiclenon-equilibrium chemical flownon-equilibrium Navier-Stokes equationsplanetary probe heat shield designsphere-cone capsule shape

Mathematics Subject Classification ID

Research exposition (monographs, survey articles) pertaining to fluid mechanics (76-02) Hypersonic flows (76K05)

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