Reduction of TSTO Hypersonic Aerodynamic Interactions Due to Diagonally-Cut Circular Cylinder Orbiter Nose-Reference-Cited by-同舟云学术

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Reduction of TSTO Hypersonic Aerodynamic Interactions Due to Diagonally-Cut Circular Cylinder Orbiter Nose

Published:2008 Issue:648 Volume:56 Page:8-14
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Ozawa Hiroshi,Hanai Katsuhisa,Nakamura Yoshiaki

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/56/648/56_648_8/_pdf

Reference13 articles.

1. 1) Dulepov, N. P., Lanshin, A. I., Sokolova, O. V. and Tjurikov, E. V.: Propulsion Systems for TSTO Airplane-Accelerators of Different Types, AIAA Paper 2001-1914, 2001.

2. 4) 中北和之:衝撃風洞における空気力及び空力加熱率の測定法について,1993年度名古屋大学修士論文.

3. Type III and type IV shock/shock interferences: theoretical and experimental aspects

Cited by 2 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. Effects of Crack on Heat Flux in Hypersonic Shock/Boundary-Layer Interaction;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010

2. Investigation on Hypersonic Shock Interacting and Boundary-Layer Separating Flowfield around Two-Stage-To-Orbit Vehicle;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008

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