Nummerical Simulation in Influence of Forward-Facing Cavity on Aerodynamic Heating of Hypersonic Vehicle-Reference-Cited by-同舟云学术

Nummerical Simulation in Influence of Forward-Facing Cavity on Aerodynamic Heating of Hypersonic Vehicle

Published:2012 Issue: Volume:29 Page:4096-4100
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Lu Haibo,Liu Weiqiang

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference10 articles.

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3. W A Engblom, D B Goldstein. Nose-Tip Surface Heat Reduction Mechanism. AIAA 96-0354, 1996.

4. Silton S I, Goldstein D B. Modeling of Nose Tip Ablation Onset in Unsteady Hypersonic Flow. AIAA 2000-0204, 2000.

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