Advance in LES Modelling: Effect of the Turbulent Schmidt Number on Supersonic Regime

Advance in LES Modelling: Effect of the Turbulent Schmidt Number on Supersonic Regime

著者名:

A. Ingenito ( DMA University of Rome, Rome, Rome, Italy )
C. Bruno ( University of Rome "La Sapienza", Rome, Rome, Italy )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

2007

発行年:

2007

通号:

2007-5633

ペーパー番号:

AIAA Paper 2007-5633

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200716 [CD-ROM 2007 Disc 16]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049508
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	43rd
会議開催地:	Cincinnati, OH
会議開催年:	2007.07.08-2007.07.11
論文注記:	43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-11, 2007

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3 テクニカルペーパー A Novel Model of Turbulent Supersonic Combustion: Development and Validation A. Ingenito, G. De Flora, C. Bruno American Institute of Aeronautics and Astronautics	9 テクニカルペーパー LES Modeling of Scramjet Combustion A. Ingenito, M. De Flora, C. Bruno, E. Giacomazzi, J. Steelant American Institute of Aeronautics and Astronautics
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6 テクニカルペーパー Supersonic Combustion: Modelling and Simulations A. Ingenito, C. Bruno, E. Giacomazzi, J. Steelant American Institute of Aeronautics and Astronautics	12 テクニカルペーパー TWO-EQUATION LOW-REYNOLDS-NUMBER TURBULENCE MODELING OF TRANSITIONAL BOUNDARY LAYER FLOWS CHARACTERISTIC OF GAS TURBINE BLADES Ph. D. Thesis. Schmidt, Rodney C. et al. National Aeronautics and Space Administration

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