Prediction and Control of Vortex Dominated and Vortex-wake Flows | 東京工業大学附属図書館文献データベース

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Prediction and Control of Vortex Dominated and Vortex-wake Flows

著者名:: Kandil, Osama ( Old Dominion Univ. )
掲載資料名:: NASA Technical Reports
発行年:: 1996
巻:: 19970005140
号:: NASA-CR-202815
パート:: NAS 1.26:202815
開始ページ:: 1
終了ページ:: 7
総ページ数:: 7
出版情報:: National Aeronautics and Space Adminstration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:	ZA00001434
論文注記:	NAG-1-994

類似資料:

1 テクニカルペーパー PREDICTION AND CONTROL OF VORTEX-DOMINATED AND VORTEX-WAKE FLOWS Kandil, Osama National Aeronautics and Space Adminstration	7 テクニカルペーパー Optimization of Active Flow Control in Transonic Aerodynamics Yagiz, Bedri, Kandil, Osama American Institute of Aeronautics and Astronautics
2 テクニカルペーパー ANALYSIS AND MITIGATION OF NUMERICAL DISSIPATION IN INVISCID AND VISCID COMPUTATION OF VORTEX-DOMINATED FLOWS kandil, Osama A. National Aeronautics and Space Adminstration	8 テクニカルペーパー Effective control of computationally simulated wing rock in subsonic flow Kandil, Osama A., Menzies, Margaret A. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー ANALYSIS AND CONTROL OF SUPERSONIC VORTEX BREAKDOWN FLOWS Kandil, Osama A. National Aeronautics and Space Adminstration	9 テクニカルペーパー EFFECTIVE CONTROL OF COMPUTATIONALLY SIMULATED WING ROCK IN SUBSONIC FLOW Kandil, Osama A., Menzies, Margaret A. National Aeronautics and Space Adminstration
4 テクニカルペーパー UNSTEADY HYBRID VORTEX TECHNIQUE FOR TRANSONIC VORTEX FLOWS AND FLUTTER APPLICATION Progress Report, 1 Jan. - 31 Kandil, Osama A. National Aeronautics and Space Administration	10 テクニカルペーパー Far-Field Turbulent Vortex-Wake/Exhaust Plume Interaction for Subsonic and HSCT Airplanes Kandil, Osama A., Adam, Ihab, Wong, Tin-Chee National Aeronautics and Space Adminstration
5 テクニカルペーパー Investigation of three-dimensional vortex-wake interaction with the ground Adam, Ihab G., Kandil, Osama A. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes Kandil, Osama A., Adam, Ihab, Wong, Tin-Chee American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing Kandil, Osama A., Menzies, Margaret A. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー NAVIER-STOKES, DYNAMICS AND AEROELASTIC COMPUTATIONS FOR VORTICAL FLOWS, BUFFET AND FLUTTER APPLICATIONS Kandil, Osama A. National Aeronautics and Space Adminstration

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