Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer

Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer

著者名:

X. Wang ( University of California, Los Angeles, Los Angeles, CA )
X. Zhong

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:

2006

発行年:

2006

通号:

2006-1107

ペーパー番号:

AIAA Paper 2006-1107

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200604 [CD-ROM 2006 Disc 4]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047219
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	44th
会議開催地:	Reno, Nevada
会議開催年:	2006.01.09-2009.01.12

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1 テクニカルペーパー Numerical Simulation of Leading Edge Receptivity of Stetson's Mach 8 Blunt Cone Stability Experiments Zhong, X., Ma, Y. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Numerical Simulation of Hypersonic Boundary Layer Receptivity and Stability on Blunt Circular Cones X. Zhong American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Numerical Simulations of Transient Growth in a Mach 15 Boundary Layer Over a Blunt Leading Edge Dong, H., Zhong, X. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges, part I: a new numerical method and validation Zhong, Xiaolin American Institute of Aeronautics and Astronautics
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