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超音速における軌道再突入実験機模型の空力特性
超音速における軌道再突入実験機模型の空力特性
Digital
文書・図像類
野田, 順一, 楯, 篤志, 渡辺, 光則, 関根, 英夫, 吉永, 崇, 秋元, 敏男, Noda, Junichi, Tate, Atsushi, Watanabe, Mitsunori, Sekine, Hideo, Yoshinaga, Takashi, Akimoto, Toshio
航空宇宙技術研究所
1996-07
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory
1300
p.1-30
Other Libraries in Japan
Subject Heading
...離バブル 抗力係数 揚力係数
縦揺れモーメント
風洞実験 orbital reentry experime...
Note (General)
...径が小さい模型の抗力係数および
縦揺れモーメント
係数の絶対値の方が、肩の曲率半径が大きい模型の値より大きい。...
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