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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20° to 90° / prepared for Langley Research Center (NASA contractor report ; 3248)

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20° to 90° / prepared for Langley Research Center (NASA contractor report ; 3248)
Microform図書
1984<YCA-NAS 1.26:3248>
National Diet Library
  • Subject HeadingSpin (Aerodynamics) -- Mathematical models Wind tunnel balances

航技研10cm×10cm磁力支持天秤装置横揺れ制御について

航技研10cm×10cm磁力支持天秤装置横揺れ制御について
Digital文書・図像類
澤田, 秀夫, 末永, 尚史, 鈴木, 孝行, 池田, 宣一, Sawada, Hideo, Suenaga, Hisashi, Suzuki, Takayuki, Ikeda, Nobukazu航空宇宙技術研究所1992-06航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1164p.1-14
Other Libraries in Japan
  • Subject Heading...test technique wind tunnel balance six degree of freedom model m...

内挿式6分力天秤の較正について　第1報:遷音速風洞における実荷重較正の現状

内挿式6分力天秤の較正について　第1報:遷音速風洞における実荷重較正の現状
Digital文書・図像類
河本, 巌, 鈴木, 弘一, 中村, 正剛, 小國, 保男, Kawamoto, Iwao, Suzuki, Koichi, Nakamura, Seigo, Oguni, Yasuo航空宇宙技術研究所1994-03航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory663p.1-40
Other Libraries in Japan
  • Subject Heading...洞試験データ処理 遷音速風洞 wind tunnel balance calibration combined load bal...

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