Heat-Shielding with Gas Injection into Boundary Layer in High Speed Flight-Reference-Cited by-同舟云学术

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Heat-Shielding with Gas Injection into Boundary Layer in High Speed Flight

Published:1972 Issue:221 Volume:20 Page:319-335
ISSN:0021-4663
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:

KUBOTA Hirotoshi

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass1969/20/221/20_221_319/_pdf

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. Study on the Injection Cooling Method for Hypersonic Flow over Flat Plate with Tile Gaps;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023

2. Film Cooling Effectiveness in High Enthalpy Flows;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007

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