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極超音速飛行実験機(HYFLEX)の空力特性
極超音速飛行実験機(HYFLEX)の空力特性
Digital
文書・図像類
航空宇宙技術研究所, National Aerospace Laboratory
航空宇宙技術研究所
1997-12
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory
1334
p.1-95
Other Libraries in Japan
Subject Heading
...characteristic
aerodynamic force coefficient
longitudinal trim stability c...
Note (General)
...nted. They are
aerodynamic force coefficient
s, longitudinal trim character...
Reached to the end of result.
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