超音速流中での二物体相互干渉の近似推算法(軸力)

Material type: 文書・図像類

Author: 近藤, 洋史ほか

Publisher: 航空宇宙技術研究所

Publication date: 1983-01

Material Format: Digital

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Note (General)：: The present study deals with an approximate method of estimating the aerodynamic interference between two paralle bodies in a supersonic flow. The for...

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Material Type: 文書・図像類
Title: 超音速流中での二物体相互干渉の近似推算法(軸力)
Author/Editor: 近藤, 洋史
KONDO, Hirofumi
Author Heading: 近藤, 洋史
KONDO, Hirofumi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1983-01
Publication Date (W3CDTF): 1983-01
Alternative Title: An Approximate Method of Estimating the Aerodynamic Interference between Two Parallel Bodies in a Supersonic Flow(Axial Force)
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-751
No. or year of volume/issue: 751
Volume: 751
Pages: 16-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): The present study deals with an approximate method of estimating the aerodynamic interference between two paralle bodies in a supersonic flow. The formulae are derived from the linearized theory. The formulae for calculating the wave drag on one body are obtained as functions of Mach number, cone semi-vertex angle, and the relative distances between bodies. Theoretical calculations are compared with wind tunnel test results, and fairly good agreement is noted between them at certain restricted regions, depending on Mach number, cone vertex angle, and relative distances between bodies. It is pointed out that the present method can easily be applied to a combination of more than two bodies.
資料番号: NALTR0751000
レポート番号: NAL TR-751
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