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検索結果 18 件

骨芽細胞の荷重負荷に起因する細胞増殖促進メカニズムの解析

骨芽細胞の荷重負荷に起因する細胞増殖促進メカニズムの解析
紙図書
浜崎, 辰夫, 東京医科歯科大学1997-1998<Y151-H09671982>
国立国会図書館
  • 件名osteoblast mechanical stress static pressure culture cell cell growth cell...

PSP measurement of stator vane surface pressures in a high speed fan [microform] / Jan Lepicovsky ([NASA contractor report] ; NASA/CR-1998-207403)

PSP measurement of stator vane surface pressures in a high speed fan [microform] / Jan Lepicovsky ([NASA contractor report] ; NASA/CR-1998-207403)
マイクロ図書
1998<YCA-NAS 1.26:207403>
国立国会図書館
  • 件名Turbomachinery Static pressure Internal flow Stators

Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel [microform] / David M. Schuster ([NASA technical memorandum] ; NASA/TM-2001-210828)

Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel [microform] / David M. Schuster ([NASA technical memorandum] ; NASA/TM-2001-210828)
マイクロ図書
2001<YCA-NAS 1.15:210828>
国立国会図書館
  • 件名...namic pressure Static pressure Viscous flow Wind tunnel test...

Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.] ([NASA contractor report] ; NASA-CR-204816)

Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.] ([NASA contractor report] ; NASA-CR-204816)
マイクロ図書
1997<YCA-NAS 1.26:204816>
国立国会図書館
  • 件名Engine inlets Ducts Ducted flow Flow visualization Pressure reduction Static pressure

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone (NASA/TM ; 1998-208723)

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone (NASA/TM ; 1998-208723)
マイクロ図書
1998<YCA-NAS 1.15:208723>
国立国会図書館
  • 件名...personic speed Static pressure Shock waves Mach number Bow w...

Study of CFD methods applied to rapidly deforming boundaries [microform] / John W. Slater and Donald Freund and Miklos Sajben

Study of CFD methods applied to rapidly deforming boundaries [microform] / John W. Slater and Donald Freund and Miklos Sajben
マイクロ図書
1997<YCA-NAS 1.15:107482>
国立国会図書館
  • 件名...w distribution Static pressure Annular ducts Boundaries

Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez (NASA contractor report ; 195438)

Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez (NASA contractor report ; 195438)
マイクロ図書
1997<YCA-NAS 1.26:195438>
国立国会図書館
  • 件名...s Manipulators Static pressure Pitch (inclination) Yaw

Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.] (NASA/TM ; 1999-206579)

Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.] (NASA/TM ; 1999-206579)
マイクロ図書
1999<YCA-NAS 1.15:206579>
国立国会図書館
  • 件名...rodynamic drag Static pressure Subsonic speed Boundary layer...

Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis (NASA technical memorandum ; 107392)

Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis (NASA technical memorandum ; 107392)
マイクロ図書
1996<YCA-NAS 1.15:107392>
国立国会図書館
  • 件名...Mass flow rate Static pressure Shock waves

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis (NASA technical memorandum ; 110300)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis (NASA technical memorandum ; 110300)
マイクロ図書
1996<YCA-NAS 1.15:110300>
国立国会図書館
  • 件名...e distribution Static pressure Engine inlets Aircraft engine...

Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin [microform] / by Paul J. Barnhart and Isaac Greber (NASA contractor report ; 202334)

Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin [microform] / by Paul J. Barnhart and Isaac Greber (NASA contractor report ; 202334)
マイクロ図書
1997<YCA-NAS 1.26:202334>
国立国会図書館
  • 件名... visualization Static pressure Dynamic pressure Wave interac...

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster (NASA technical memorandum ; 107274) (ICOMP ; 96-6)

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster (NASA technical memorandum ; 107274) (ICOMP ; 96-6)
マイクロ図書
1996<YCA-NAS 1.15:107274>
国立国会図書館
  • 件名...e distribution Static pressure Computational grids Hypersoni...

Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas (NASA contractor report ; 198052)

Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas (NASA contractor report ; 198052)
マイクロ図書
1996<YCA-NAS 1.26:198052>
国立国会図書館
  • 件名...Inlet pressure Static pressure Flow measurement Gas turbine ...

高速飛行実証(フェーズ2)に関する空力関連検討集

高速飛行実証(フェーズ2)に関する空力関連検討集
デジタル文書・図像類
上野, 真, 廣谷, 智成, 重見, 仁, 柳原, 正明, 若井, 洋, 岩田, 徹, Ueno, Makoto, Hirotani, Tomonari, Shigemi, Masashi, Yanagihara, Masaaki, Wakai, Hiroshi, Iwata, Toru宇宙航空研究開発機構2005-03-31宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-04-043
全国の図書館
  • 件名...le sweep angle static pressure dynamic pressure
  • 一般注記... by additional static pressure holes on the stem surface of ...

ムービングベルト式地面効果試験装置

ムービングベルト式地面効果試験装置
デジタル文書・図像類
野中, 修, 萱場, 重男, 林, 良生, Nonaka, Osamu, Kayaba, Shigeo, Hayashi, Yoshio航空宇宙技術研究所1998-02航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory724p.1-30
全国の図書館
  • 件名... layer suction static pressure distribution turbulent distri...
  • 一般注記...indicated: (1) static pressure distribution along the wind t...

CAD設計によるUSB-STOL機半裁模型のエンジン後流測定:排気流偏向特性に対するエンジン間隔の影響

CAD設計によるUSB-STOL機半裁模型のエンジン後流測定:排気流偏向特性に対するエンジン間隔の影響
デジタル文書・図像類
藤枝, 郭俊, 藤田, 敏美, 岩崎, 昭人, 高橋, ひとし, 奥山, 政広, Fujieda, Hirotoshi, Fujita, Toshimi, Iwasaki, Akihito, Takahashi, Hitoshi, Okuyama, Masahiro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 Laboratory682p.1-21
全国の図書館
  • 件名...characteristic static pressure distribution

吸い込みのある2次元自然層流翼の高亜音速、高Re数風洞試験

吸い込みのある2次元自然層流翼の高亜音速、高Re数風洞試験
デジタル文書・図像類
野口, 正芳, 佐藤, 衛, 神田, 宏, 石田, 洋治, Noguchi, Masayoshi, Sato, Mamoru, Kanda, Hiroshi, Ishida, Yoji航空宇宙技術研究所1993-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1204p.1-14
全国の図書館
  • 件名...d wall suction static pressure measurement

HOPE小型自動着陸実験機8.9％模型の低速風洞試験

HOPE小型自動着陸実験機8.9％模型の低速風洞試験
デジタル文書・図像類
重見, 仁, 岩崎, 昭人, 藤田, 敏美, 大貫, 武, 李家, 賢一, 中安, 英彦, 加納, 康臣, Shigemi, Masashi, Iwasaki, Akihito, Fujita, Toshimi, Onuki, Takeshi, Rinoie, Kenichi, Nakayasu, Hidehiko, Kano, Yasuomi航空宇宙技術研究所1993-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1215p.1-23
全国の図書館
  • 件名...nt measurement static pressure distribution measurement spac...
  • 一般注記...ibution of the static pressure on both sides of the wings; a...

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