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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 Laboratory1334p.1-95
Other Libraries in Japan
  • Subject Heading...ce coefficient longitudinal trim stability control derivative ...
  • Note (General)... coefficients, longitudinal trim characteristics, stability an...

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