Computational Aeroacoustics of the Coaxial Flow Exhaust System of a Gas Turbine Engine.

Computational Aeroacoustics of the Coaxial Flow Exhaust System of a Gas Turbine Engine.

著者名:

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : GT

シリーズ巻号:

2007

発行年:

2007

通号:

GT2007-28193

ペーパー番号:

GT2007-28193

総ページ数:

9

出版情報:

New York, NY: American Society of Mechanical Engineers

言語:

英語

請求記号:

A11800

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052166
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2007: Power for Land, Sea and Air
回次:	2007
会議開催地:	Montreal, Canada
会議開催年:	2007.05.14-2007.05.17
論文注記:	ASME Turbo Expo 2007: Power for Land, Sea and Air, Montreal, Canada, 2007.5.14-2007.05.17

類似資料:

1 国際会議録 Computational Aeroacoustics of the Coaxial Flow Exhaust System of a Gas Turbine Engine Ephraim J. Gutmark, Mihai Mihaescu, Laszlo Fuchs American Society of Mechanical Engineers	7 テクニカルペーパー Coaxial Jet Noise Prediction: Grid Resolution Effect on the Numerical Solution Mihaescu, M., Szasz, R., Fuchs, L., Gutmark, E. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Computational Aeroacoustics of a Separate Flow Exhaust System with Eccentric Inner Nozzle M. Mihaescu, E. Gutmark, R. Szasz, L. Fuchs, S. Martens American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Experimental Study of a Flameless Gas Turbine Combustor. Li, G., Gutmark, E.J., Overman, N., Cornwell, M., Stankovic, D., Fuchs, L. American Society of Mechanical Engineers
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5 テクニカルペーパー Flow and Acoustics of a Coaxial Nozzle: a Sensitivity Study to the Inlet Boundary Conditions M. Mihaescu, E. Gutmark, R. Szasz, L. Fuchs American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Large Eddy Simulation of the Flow in a Pediatric Airway with Subglottic Stenosis M. Mihaescu., E. Gutmark, R. Elluru., J. Willging American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Numerical Investigations of the Acoustics of a Coaxial Nozzle Mihaescu, M., Szasz, R., Fuchs, L., Gutmark, E. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー The Effect of Fuel Injector Geometry on The Flow Structure of a Swirl Stabilized Gas Turbine Burner. Anning, G.H.G., Gutmark, E.J. American Institute of Aeronautics and Astronautics

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