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

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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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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
Volume: 660
Pages: 1-14
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: jpn
Subject Heading: 空力加熱率
熱伝達率
極超音速空気力学
極超音速風洞
風洞試験技術
模型投入装置
カロリーメータ法
感温塗料法
相変化塗料法
赤外線放射温度
空力干渉
計測法
球頭円錐模型
航空宇宙技術研究所
NAL
aerodynamic heating rate
heat transfer rate
hypersonic aerodynamics
hypersonic wind tunnel
wind tunnel testing technique
model injection system
calorie meter method
temperature sensitive paint method
phase change paint method
infrared radiation temperature
aerodynamic interference
instrumentation technique
spherical nose cone model
National Aerospace Laboratory
Target Audience: 一般
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 measurement used in hypersonic wind tunnels are briefly summarized and the characteristics of a new rapid injection system to improve the accuracy of aerodynamic heating rate measurement in test models are also described. Experimental studies using this system for six sphere-cone models were conducted at a Mach number of 7.1 in the 50 cm NAL hypersonic wind tunnel. Test results showed that this system was able to improve the accuracy of aerodynamic heating rate measurement in comparison with the existing system.
資料番号: AA0004148000
レポート番号: NAL TM-660
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=41127&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=41127&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ