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検索結果 7 件

Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets [microform] / Bernhard H. Anderson, Henry D. Baust, Johan Agrell (NASA/TM-2002-212000)

Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets [microform] / Bernhard H. Anderson, Henry D. Baust, Johan Agrell (NASA/TM-2002-212000)
マイクロ図書
2002<YCA-NAS 1.15:2002-212000>
国立国会図書館
  • 件名...tical analysis Pressure recovery

A computational-experimental development of vortex generator use for a transitioning S-diffuser [microform] / Bruce J. Wendt and Julianne C. Dudek (NASA technical memorandum ; 107357)

A computational-experimental development of vortex generator use for a transitioning S-diffuser [microform] / Bruce J. Wendt and Julianne C. Dudek (NASA technical memorandum ; 107357)
マイクロ図書
1996<YCA-NAS 1.15:107357>
国立国会図書館
  • 件名Vortex generators Diffusers Navier-Stokes equation Pressure recovery

IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart ([NASA contractor report] ; NASA CR-204130)

IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart ([NASA contractor report] ; NASA CR-204130)
マイクロ図書
1997<YCA-NAS 1.26:204130>
国立国会図書館
  • 件名Aerodynamic drag Pressure recovery Inlet flow Engine inlets Reli...

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60⁰ angle of attack [microform] : contract NAS 3-26617 / Kevin R. Walsh ... [et al.] (NASA technical memorandum ; 104329)

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60⁰ angle of attack [microform] : contract NAS 3-26617 / Kevin R. Walsh ... [et al.] (NASA technical memorandum ; 104329)
マイクロ図書
1997<YCA-NAS 1.15:104329>
国立国会図書館
  • 件名...fluid dynamics Pressure recovery Subsonic speed

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel [microform] : progress report on the D.S.M.A. design / P.S. Barna (NASA contractor report ; 198311)

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel [microform] : progress report on the D.S.M.A. design / P.S. Barna (NASA contractor report ; 198311)
マイクロ図書
1995<YCA-NAS 1.26:198311>
国立国会図書館
  • 件名...zation Blowing Pressure recovery Diffusers Wind tunnel models ...

マッハ4におけるスクラムジェット空気取入口の実験(その1)

マッハ4におけるスクラムジェット空気取入口の実験(その1)
デジタル文書・図像類
苅田, 丈士, 小室, 智幸, 升谷, 五郎, 工藤, 賢司, 村上, 淳郎, 谷, 香一郎, 若松, 義男, 鎮西, 信夫, KANDA, Takeshi, KOMURO, Tomoyuki, MASUYA, Goro, KUDO, Kenji, MURAKAMI, Atsuo, TANI, Kouichiro, WAKAMATSU, Yoshio, CHINZEI, NOBUO航空宇宙技術研究所1991-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-11371137p.50-
全国の図書館
  • 件名scramjet; inlet; supersonic flow; sweep angle; total pressure recovery
  • 一般注記...atio and total pressure recovery were found to ......aximized total pressure recovery were obtained. 資料番号: NALTR113...

超音速内部流におけるキャビティ抽気およびその形状の空力特性への影響

超音速内部流におけるキャビティ抽気およびその形状の空力特性への影響
デジタル文書・図像類
村上, 哲, 進藤, 重美, 小宮山, 文男, 坂田, 公夫, Murakami, Akira, Shindo, Shigemi, Komiyama, Fumio, Sakata, Kimio航空宇宙技術研究所1994-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1247p.1-16
全国の図書館
  • 件名...re measurement pressure recovery cavity pressure internal flow...
  • 一般注記...ir-intake. The pressure recovery characteristic......aggravated the pressure recovery. The cavity co......or the maximum pressure recovery depended on the cavity config...

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