Determination of Surface Pressure and Temperature Distributions of Hypersonic Waveriders-Reference-Cited by-同舟云学术

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Determination of Surface Pressure and Temperature Distributions of Hypersonic Waveriders

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Zien Tse-Fou¹

Affiliation:

1. Naval Surface Warfare Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6574

Reference10 articles.

1. 2Zien, T. F. "A Class of Three Dimensional Optimum Wings in Hypersonic Flow". Ph. D dissertation, 1967, Graduate Aeronautical LaboratoryofCaliforniaInstituteofTechnology, Pasadena, California

2. 3VanDyke,M.D."AStudyofHypersonicSmall-DisturbanceTheory",Rept.1194,1954,NACA.

3. A class of three-dimensional, optimum hypersonic wings.

4. Modeling of Hypersonic Melting Ablation Near Stagnation Point and Extension to Waveriders

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Recent Developments in Modeling Hypersonic Melting Ablation;6th AIAA Theoretical Fluid Mechanics Conference;2011-06-14

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