A Comparison of Scramjet Engine Performances of Various Cycles

Material type: 文書・図像類

Author: 苅田, 丈士ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-11

Material Format: Digital

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Note (General)：: Assuming an airframe-integrated hydrogen fueled scramjet engine, we compared the performances of engines of various engine cycles : an expander cycle,...

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Material Type: 文書・図像類
Title: A Comparison of Scramjet Engine Performances of Various Cycles
Author/Editor: 苅田, 丈士
升谷, 五郎
若松, 義男
鎮西, 信夫
冠, 昭夫
KANDA, Takeshi
MASUYA, Goro
WAKAMATSU, Yoshio
CHINZEI, NOBUO
KANMURI, Akio
Author Heading: 苅田, 丈士
升谷, 五郎
若松, 義男
鎮西, 信夫
冠, 昭夫
KANDA, Takeshi
MASUYA, Goro
WAKAMATSU, Yoshio
CHINZEI, NOBUO
KANMURI, Akio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-11
Publication Date (W3CDTF): 1989-11
Alternative Title: スクラムジェットエンジンサイクル性能比較
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1042
No. or year of volume/issue: 1042
Volume: 1042
Pages: 14-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): Assuming an airframe-integrated hydrogen fueled scramjet engine, we compared the performances of engines of various engine cycles : an expander cycle, a staged combustion cycle, a coolant bleed cycle, and a gas generator cycle. Each engine was regeneratively cooled by liquid hydrogen. Effects of flight Mach number, flight dynamic pressure, and fuel injection to air dynamic pressure ratio were examined as related to the power balance of the propellant feed line. It follows that the system pressure of the closed loop cycle increases and the specific impulse of the open loop cycle decreases with increasing flight Mach number, flight dynamic pressure, or fuel injection to air dynamic pressure ratio, i.e., with increasing fuel injector manifold pressure. Of the four cycles, the coolant bleed cycle shows well balanced engine performance, keeping the system pressure within a reasonable range.
資料番号: NALTR1042000
レポート番号: NAL TR-1042
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45301&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45301&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