Role of Turbulent Prandtl Number on Heat Flux at Hypersonic Mach Numbers

Role of Turbulent Prandtl Number on Heat Flux at Hypersonic Mach Numbers

著者名:

Xiao, X. ( North Carolina State University, Raleigh, NC )
Edwards, J.
Hassan, H.
Gaffney, R. ( NASA Langley Research Center, Hampton, VA )

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:

2005-1098

ペーパー番号:

AIAA Paper 2005-1098

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200503 [CD-ROM 2005 Disc 3]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001618
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

類似資料:

1 テクニカルペーパー Modeling Scramjet Flows with Variable Turbulent Prandtl and Schmidt Numbers X. Xiao, H. Hassan, R. Baurle American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Turbulence Modeling for Scramjet Applications Keistler, P., Gaffney, R., Xiao, X., Hassan, H. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー A Variable Turbulent Schmidt Number Formulation for Scramjet Application Xiao, X., Edwards, J., Hassan, H., Cutler, A. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Hybrid LES/RANS Simulation of a Shock Wave/Boundary Layer Interaction. Fan, T.C., Xiao, X., Edwards, J.R., Hassan, H.A., Baurle, R.A. American Institute of Aeronautics and Astronautics
3 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	9 テクニカルペーパー Development of an In-Cylinder Heat Transfer Model with Compressibility Effects on Turbulent Prandtl Number, Eddy Viscosity Ratio and Kinematic Viscosity … Park, H.J., Assanis, D.N., Jung, D. Society of Automotive Engineers
4 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	10 テクニカルペーパー Simulation of Transitional Flow Over an Elliptic Cone at Mach 8 Using a One-Equation Transition/Turbulence Model Malechuk, A.M., Edwards, J.R., Hassan, H.A. American Institute of Aeronautics and Astronautics
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 ROLE OF BYPASS TRANSITION IN CONVENTIONAL HYPERSONIC FACILITIES McDaniel,R.D., Hassan,H.A. American Institute of Aeronautics and Astronautics
6 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	12 テクニカルペーパー Role of Chemistry/Turbulence Interactions in 3d Supersonic Combustion P. Keistler, H. Hassan, X. Xiao American Institute of Aeronautics and Astronautics

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