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極超音速風洞模型高速投入装置による空力加熱測定精度向上の試み

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極超音速風洞模型高速投入装置による空力加熱測定精度向上の試み

Material type
文書・図像類
Author
小山, 忠勇ほか
Publisher
航空宇宙技術研究所
Publication date
1993-11
Material Format
Digital
Capacity, size, etc.
-
NDC
-
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Notes on use

Note (General)：

航空宇宙技術研究所(NAL)50cm極超音速風洞における空力加熱率分布測定法の概要と測定精度を向上させるため開発した模型高速投入装置の詳細ならびに球状鈍頭円錐模型による評価試験について述べた。In this paper, some methods of heat transfer measureme...

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Digital

Material Type
文書・図像類
Title
極超音速風洞模型高速投入装置による空力加熱測定精度向上の試み
Author/Editor
小山, 忠勇
Koyama, Tadao
Author Heading
小山, 忠勇
Koyama, Tadao
Publication, Distribution, etc.
航空宇宙技術研究所
Publication Date
1993-11
Publication Date (W3CDTF)
1993-11
Alternative Title
Improved accuracy of aerodynamic heating rate measurement by use of a new rapid injection system for test models in NAL hypersonic wind tunnel
Periodical title
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
No. or year of volume/issue
660