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検索結果 7 件

Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck ([NASA technical memorandum] ; NASA/TM-2000-210541)

Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck ([NASA technical memorandum] ; NASA/TM-2000-210541)
マイクロ図書
2000<YCA-NAS 1.15:210541>
国立国会図書館
  • 件名Reynolds number Ailerons Spoilers Lateral control

In-flight transport performance optimization [microform] : an experimental flight research program and an operational scenario / Glenn Gilyard (NASA/TM ; 97-206229)

In-flight transport performance optimization [microform] : an experimental flight research program and an operational scenario / Glenn Gilyard (NASA/TM ; 97-206229)
マイクロ図書
1997<YCA-NAS 1.15:206229>
国立国会図書館
  • 件名...g Optimization Ailerons Real time operation Aerodynam...

Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration / Wendell W. Kelley, Einar K. Enevoldson. (NASA technical memorandum ; 81972)

Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration / Wendell W. Kelley, Einar K. Enevoldson. (NASA technical memorandum ; 81972)
紙図書
National Aeronautics and Space Administration, Scientific and Technical Information Branch1981.<NC125-22>
国立国会図書館
  • 件名Ailerons. Airplanes, Military -- Fligh...

Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines / Wichita State University ; W. H. Wentz, M.H. Snyder, and J.T. Calhoun.

Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines / Wichita State University ; W. H. Wentz, M.H. Snyder, and J.T. Calhoun.
紙図書
U.S. Dept. of Energy, Distributed Solar Technology Division1980.<ND158-53>
国立国会図書館
  • 件名Turbines -- Aerodynamics. Airplanes -- Control surfaces. Ailerons. Spoilers (Airplanes)

Unsteady shock wave motions on a thin airfoil at transonic speeds caused by aileron oscillations

Unsteady shock wave motions on a thin airfoil at transonic speeds caused by aileron oscillations
デジタル文書・図像類
玉山, 雅人, 中道, 二郎, Tamayama, Masato, Nakamichi, Jiro宇宙航空研究開発機構2004-03-25宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-03-017E
全国の図書館

Numerical flutter simulation: Application to structural design of main surface of SST experimental aircraft

Numerical flutter simulation: Application to structural design of main surface of SST experimental aircraft
デジタル文書・図像類
中道, 二郎, Kheirandish, Hamid Reza, Nakamichi, Jiro航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory49Tp.179-182
全国の図書館

光学式3次元位置測定装置による風洞内動的模型の位置測定

光学式3次元位置測定装置による風洞内動的模型の位置測定
デジタル文書・図像類
野中, 修, 鈴木, 誠三, Nonaka, Osamu, Suzuki, Seizo航空宇宙技術研究所1995-04航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory681p.1-21
全国の図書館

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