Multiple Temperature Kinetic Model for Continuum and Near Continuum Flows

Multiple Temperature Kinetic Model for Continuum and Near Continuum Flows

著者名:

K. Xu ( Hong Kong University of Science and Technology, Hong Kong )
H. Liu
J. Jiang

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:

2007

発行年:

2007

通号:

2007-0616

ペーパー番号:

AIAA Paper 2007-616

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200703 [CD-ROM 2007 Disc 3]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050742
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	45th
会議開催地:	Reno, Nevada
会議開催年:	2007.01.08-2007.01.11

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2 テクニカルペーパー Gas Kinetic Scheme for Continuum and Near-Continuum Hypersonic Flows W. Liao, L. Luo, K. Xu American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Investigation of Flow in a Steam Turbine Exhaust Hood With/Without Turbine Exit Conditions Simulated. Liu, J., Cui, Y., Jiang, H. American Society of Mechanical Engineers
3 テクニカルペーパー Multiple Temperature Kinetic Model for Non-Equilibrium Flow Computations K. Xu, X. He, C. Cai American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Simulate Hypersonic Nonequlibrium Flow Using Kinetic Models J. Shang, H. Yan, S. Surzhikov American Institute of Aeronautics and Astronautics
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