المؤلفون: Fujii, Keisuke, Watanabe, Shigeya, Shirouzu, Masao, Inoue, Yasutoshi, Kurotaki, Takuji, Koyama, Tadao, Tsuda, Shoichi, Hirabayashi, Noriaki

المصدر: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1415:1-65

مصطلحات موضوعية: 空気解離, 境界層遷移, elevon part, catalytic wall, Hypersonic Flight Experiment, 計算流体力学, computational fluid dynamics, HYFLEX vehicle, 触媒性壁, 極超音速飛行実験, CFD calculation, afterbody, 空力加熱測定, stagnation region, エレボン部, 後部胴体, aerodynamic heating, air dissociation, CFD計算, laminarization, HYFLEX機, 層流化, boundary layer transition, 澱み点近傍

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::0f652a627859d93efc86773bfe262a80
http://id.nii.ac.jp/1696/00041478/