鈍頭円錐模型の高エンタルピ空力試験

Material type: 文書・図像類

Author: 佐藤, 和雄ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-11-01

Material Format: Digital

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Note (General)：: In the present paper, two blunt cone models with 15 degrees of half angle were tested in a high enthalpy shock tunnel to investigate fundamental real ...

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Material Type: 文書・図像類
Title: 鈍頭円錐模型の高エンタルピ空力試験
Author/Editor: 佐藤, 和雄
小室, 智幸
高橋, 政浩
橋本, 時忠
丹野, 英幸
伊藤, 勝宏
Sato, Kazuo
Komuro, Tomoyuki
Takahashi, Masahiro
Hashimoto, Tokitada
Tanno, Hideyuki
Ito, Katsuhiro
Author Heading: 佐藤, 和雄
小室, 智幸
高橋, 政浩
橋本, 時忠
丹野, 英幸
伊藤, 勝宏
Sato, Kazuo
Komuro, Tomoyuki
Takahashi, Masahiro
Hashimoto, Tokitada
Tanno, Hideyuki
Ito, Katsuhiro
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-11-01
Publication Date (W3CDTF): 2006-11-01
Alternative Title: An experimental study of force measurements of blunt cone models in high enthalpy shock tunnel HIEST
Periodical title: 宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
No. or year of volume/issue: JAXA-SP-06-006
Volume: JAXA-SP-06-006
Pages: 99-102
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 鈍頭体
高エンタルピ衝撃風洞
空力特性
大気圏再突入
再突入機
空力試験
空力加熱
計算流体力学
計算機シミュレーション
熱力学的平衡
blunt body
high enthalpy shock tunnel
aerodynamic characteristic
atmospheric reentry
reentry vehicle
aerodynamic test
aerodynamic heating
computational fluid dynamics
computerized simulation
thermodynamic equilibrium
Target Audience: 一般
Note (General): In the present paper, two blunt cone models with 15 degrees of half angle were tested in a high enthalpy shock tunnel to investigate fundamental real gas effect on high enthalpy aerodynamic characteristics. The curvature radius of the tip of model are R = 20 mm and R = 50 mm. The tests were carried out at 4 MJ/kg-14 MJ/kg of stagnation enthalpy and the axial forces were measured by the force balance with acceleration compensation. The present results were compared with the results obtained by calculation of CFD (Computerized Fluid Dynamics). From the comparison between the experimental results and the results of CFD the real gas effect on axial force was discussed.
資料番号: AA0049500021
レポート番号: JAXA-SP-06-006
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6005&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6005&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