タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-987
一般注記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
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース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