A Variable Turbulent Schmidt Number Formulation for Scramjet Application

A Variable Turbulent Schmidt Number Formulation for Scramjet Application

著者名:

Xiao, X. ( North Carolina State University, Raleigh, NC )
Edwards, J.
Hassan, H.
Cutler, A. ( George Washington University, Raleigh, NC )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

43rd

発行年:

2005

通号:

2005-1099

ペーパー番号:

AIAA Paper 2005-1099

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200501 [CD-ROM 2005 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001616
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	43rd
会議開催地:	Reno, Nevada
会議開催年:	2005.01.10-2005.01.13

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1 テクニカルペーパー Simulation of Supersonic Combustion Using Variable Turbulent Prandtl/Schmidt Number Formulation P. Keistler, X. Xiao, H. Hassan, C. Rodriguez American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Investigation of Flow Dependent Blending Functions in Hybrid LES/RANS Simulations. Xiao, X., Edwards, J.R., Hassan, H.A. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Role of Turbulent Prandtl Number on Heat Flux at Hypersonic Mach Numbers Xiao, X., Edwards, J., Hassan, H., Gaffney, R. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー TRANSITIONAL FLOW OVER AN ELLIPTIC CONE AT MACH 8 Xiao,X., Edwards,J.R., Hassan,H.A. American Institute of Aeronautics and Astronautics
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5 テクニカルペーパー Hybrid Large Eddy/Reynolds-Averaged Navier-Stokes Simulation of Mach 8.3 Flow over a Flat Plate Edwards, J., Xiao, X., Hassan, H. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Drag reduction of supersonic cavities via mass injection with applications to scramjets Quinn, J.E., Cutler, A.D., Northam, G.B. American Institute of Aeronautics and Astronautics
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