Calculation of Scramjet Performance

Material type: 文書・図像類

Author: 升谷, 五郎ほか

Publisher: 航空宇宙技術研究所

Publication date: 1988-07

Material Format: Digital

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Note (General)：: In this paper, the performance of an airframe-integrated scramjet engine is calculated using a quasi-one-dimensional model. The forebody of the airfra...

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Material Type: 文書・図像類
Title: Calculation of Scramjet Performance
Author/Editor: 升谷, 五郎
若松, 義男
MASUYA, Goro
WAKAMATSU, Yoshio
Author Heading: 升谷, 五郎
若松, 義男
MASUYA, Goro
WAKAMATSU, Yoshio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-07
Publication Date (W3CDTF): 1988-07
Alternative Title: スクラムジェットの性能計算
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-987
No. or year of volume/issue: 987
Volume: 987
Pages: 15-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): In this paper, the performance of an airframe-integrated scramjet engine is calculated using a quasi-one-dimensional model. The forebody of the airframe is approximated as a cone. Experimental data correlations are used to estimate pressure recovery and capture area of the inlet. Assuming mixing controlled combustion, the NASA’s empirical relation for fuel mixing efficiency is employed to give the corresponding combustion efficiency distribution. The calculated results serve as engine data for a flight analysis of a space plane. The analysis is being extended to analyze overall engine cycles including subsystems for engine/airframe cooling and fuel supply.
資料番号: NALTR0987000
レポート番号: NAL TR-987
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45246&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45246&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