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検索結果 20 件

Liquid Film Formation and Heat Transfer Characteristics of a Liquid Jet Obliquely Impinging onto a Wall

Liquid Film Formation and Heat Transfer Characteristics of a Liquid Jet Obliquely Impinging onto a Wall
デジタル博士論文障害者向け資料あり
Sako, Noritaka2023-03-23
インターネットで読める国立国会図書館全国の図書館
  • 件名Liquid Film Cooling Oblique Jet Impingement Quenc...

Film cooling flow effects on post-combustor trace chemistry [microform] / Thomas Wey, Nan-Suey Liu (NASA/TM-2003-212018)

Film cooling flow effects on post-combustor trace chemistry [microform] / Thomas Wey, Nan-Suey Liu (NASA/TM-2003-212018)
マイクロ図書
2003<YCA-NAS 1.15:2002-212018>
国立国会図書館
  • 件名Film cooling Emission

Coarse grid modeling of turbine film cooling flows using volumetric source terms [microform] / James D. Heidmann, Scott D. Hunter ([NASA technical memorandum] ; NASA/TM-2001-210817)

Coarse grid modeling of turbine film cooling flows using volumetric source terms [microform] / James D. Heidmann, Scott D. Hunter ([NASA technical memorandum] ; NASA/TM-2001-210817)
マイクロ図書
2001<YCA-NAS 1.15:210817>
国立国会図書館
  • 件名Computer aided design Film cooling Flow distribution Multiblock ...

Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed [microform] / Douglas Thurman, Philip Poinsatte (NASA/TM ; 2000-209772)

Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed [microform] / Douglas Thurman, Philip Poinsatte (NASA/TM ; 2000-209772)
マイクロ図書
2000<YCA-NAS 1.15:209772>
国立国会図書館
  • 件名Heat transfer Temperature measurements Film cooling Ribs (Supports) Turbine blade...

Heat transfer on a film-cooled blade [microform] : effect of hole physics : prepared under contract NAS3-27571 / Vijay K. Garg, David L. Rigby ([NASA contractor report] ; NASA/CR--1998-206609)

Heat transfer on a film-cooled blade [microform] : effect of hole physics : prepared under contract NAS3-27571 / Vijay K. Garg, David L. Rigby ([NASA contractor report] ; NASA/CR--1998-206609)
マイクロ図書
1998<YCA-NAS 1.26:206609>
国立国会図書館
  • 件名Film cooling Coolants Heat transfer Heat t...

Large eddy simulations and turbulence modeling for film cooling [microform] / Sumanta Acharya ([NASA contractor report] ; NASA/CR-1999-209310)

Large eddy simulations and turbulence modeling for film cooling [microform] / Sumanta Acharya ([NASA contractor report] ; NASA/CR-1999-209310)
マイクロ図書
1999<YCA-NAS 1.26:209310>
国立国会図書館
  • 件名Large eddy simulation Turbulence models Film cooling Research Mathematical models

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler (NASA/TM ; 208146)

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler (NASA/TM ; 208146)
マイクロ図書
1997<YCA-NAS 1.15:208146>
国立国会図書館
  • 件名...Turbine blades Film cooling Hole geometry (Mechanics) Coo...

Effect of coolant temperature and mass flow on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler (NASA-TM ; 112760)

Effect of coolant temperature and mass flow on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler (NASA-TM ; 112760)
マイクロ図書
1997<YCA-NAS 1.15:112760>
国立国会図書館
  • 件名...on (Mechanics) Film cooling Compressibility

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
デジタル博士論文障害者向け資料あり
Wan, Aizon Bin W Ghopa岩手大学2013-09-01
国立国会図書館
  • 件名...y flow endwall film cooling leakage flow purge flow heat ...
  • 一般注記... a function of film cooling. Chapter 1 giv......ut the need of film cooling to protect the...... determine the film cooling effectiveness, η and the heat...

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
デジタル博士論文障害者向け資料あり
Wan, Aizon Bin W Ghopa岩手大学2013
国立国会図書館
  • 件名...y flow endwall film cooling leakage flow purge flow heat ...
  • 一般注記... a function of film cooling. Chapter 1 giv......ut the need of film cooling to protect the...... determine the film cooling effectiveness, η and the heat...

Experimental study of vane heat transfer and film cooling at elevated levels of turbulence [microform] / Forrest E. Ames (NASA contractor report ; 198525)

Experimental study of vane heat transfer and film cooling at elevated levels of turbulence [microform] / Forrest E. Ames (NASA contractor report ; 198525)
マイクロ図書
1996<YCA-NAS 1.26:198525>
国立国会図書館
  • 件名Gas turbines Vanes Film cooling Heat transfer Hole distributi...

The effect of wake passing on turbine blade film cooling [microform] / James David Heidmann (NASA technical memorandum ; 107380)

The effect of wake passing on turbine blade film cooling [microform] / James David Heidmann (NASA technical memorandum ; 107380)
マイクロ図書
1996<YCA-NAS 1.15:107380>
国立国会図書館
  • 件名Turbine blades Film cooling Wakes Navier-Stokes equation ...

Heat transfer on a film-cooled rotating blade [microform] / Vijay K. Garg ([NASA contractor report] ; NASA/CR-1999-209301)

Heat transfer on a film-cooled rotating blade [microform] / Vijay K. Garg ([NASA contractor report] ; NASA/CR-1999-209301)
マイクロ図書
1999<YCA-NAS 1.26:209301>
国立国会図書館
  • 件名...nsional models Film cooling Turbulent flow K-omega turbul...

NASA flow field analysis [microform] : final report / Charles L. Merkle ([NASA contractor report] ; NASA-CR-201532)

NASA flow field analysis [microform] : final report / Charles L. Merkle ([NASA contractor report] ; NASA-CR-201532)
マイクロ図書
1996<YCA-NAS 1.26:201532>
国立国会図書館
  • 件名...oxygen engines Film cooling Regenerative cooling

A numerical study of the effect of wake passing on turbine blade film cooling [microform] / James D. Heidmann (NASA technical memorandum ; 107077)

A numerical study of the effect of wake passing on turbine blade film cooling [microform] / James D. Heidmann (NASA technical memorandum ; 107077)
マイクロ図書
1995<YCA-NAS 1.15:107077>
国立国会図書館
  • 件名...tational grids Film cooling Finite difference theory Flow...

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
デジタル博士論文
Wan, Aizon Bin W Ghopa岩手大学2013p.1-154
インターネットで読める全国の図書館
  • 件名...y flow endwall film cooling leakage flow purge flow heat ...
  • 一般注記... a function of film cooling. Chapter 1 giv......ut the need of film cooling to protect the...... determine the film cooling effectiveness, η and the heat...

衝撃波干渉を伴う超音速フィルム冷却の実験　第2報

衝撃波干渉を伴う超音速フィルム冷却の実験　第2報
デジタル文書・図像類
小野, 文衛, 苅田, 丈士, 斎藤, 俊仁, 若松, 義男, Ono, Fumiei, Kanda, Takeshi, Saito, Toshihito, Wakamatsu, Yoshio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 Laboratory1340p.1-12
全国の図書館
  • 件名...eld supersonic film cooling shock wave interaction slot i...
  • 一般注記...した。 Supersonic film cooling was tested in ......ecrease of the film cooling effectiveness was mainly due ...
  • 並列タイトル等（連結）Experimental studies of supersonic film cooling with shock wave interaction, ...

流れの可視化用小型回流水槽

流れの可視化用小型回流水槽
デジタル文書・図像類
進藤, 重美, 柳, 良二, 三村, 富嗣雄, 坂田, 公夫, Shindo, Shigemi, Yanagi, Ryoji, Mimura, Fujio, Sakata, Kimio航空宇宙技術研究所1995-08航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory686p.1-38
全国の図書館
  • 件名...mics tank test film cooling turbine blade curved surface ...
  • 一般注記...annel, such as film cooling of a turbine airfoil, flow ar...

衝撃波干渉を伴う超音速フィルム冷却の実験

衝撃波干渉を伴う超音速フィルム冷却の実験
デジタル文書・図像類
小野, 文衛, 苅田, 丈士, 高橋, 政浩, 斎藤, 俊仁, 若松, 義男, Ono, Fumiei, Kanda, Takeshi, Takahashi, Masahiro, Saito, Toshihito, Wakamatsu, Yoshio航空宇宙技術研究所1995-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1276p.1-13
全国の図書館
  • 件名... 断熱壁面 温度分布 衝撃波 film cooling turbulent mixing slot injecti...
  • 一般注記...れた。 Supersonic film cooling was tested in ...... shock wave on film cooling. The coolant w......not reduce the film cooling effectiveness.......iveness of the film cooling in the restricted region. The...
  • 並列タイトル等（連結）Experimental studies of supersonic film cooling with shock wave interaction

フィルム冷却を用いたスクラムジェットエンジンの性能計算

フィルム冷却を用いたスクラムジェットエンジンの性能計算
デジタル文書・図像類
小野, 文衛, 苅田, 丈士, 升谷, 五郎, 斎藤, 俊仁, 若松, 義男, Ono, Fumiei, Kanda, Takeshi, Masuya, Goro, Saito, Toshihito, Wakamatsu, Yoshio航空宇宙技術研究所1994-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1242p.1-14
全国の図書館
  • 件名...cramjet engine film cooling regenerative heat cooling sup...
  • 一般注記...冷却剤になることが分かった。 Film cooling was modeled to...... the slot. The film cooling model was inte......combination of film cooling and regenerati......combination of film cooling and regenerati......combination of film cooling and regenerati......the coolant of film cooling. 資料番号: AA0000102000 レポート番号: N...
  • 並列タイトル等（連結）Effect of film cooling/regenerative cooling on scram...

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