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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...characteristic aerodynamic force coefficient longitudinal trim stability c...
  • Note (General)...nted. They are aerodynamic force coefficients, longitudinal trim character...

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