Numerical Investigation of Transitional Flows over a NACA0012 Airfoil.

Numerical Investigation of Transitional Flows over a NACA0012 Airfoil.

著者名:

掲載資料名:

2008 World Aviation Congress and Exposition : SAE technical paper

シリーズ名:

Society of Automotive Engineers technical paper series

シリーズ巻号:

2008

発行年:

2008

通号:

2008-01-2250

ペーパー番号:

2008-01-2250

総ページ数:

7

出版情報:

Warrendale, Penn.: Society of Automotive Engineers

ISSN:

01487191

言語:

英語

請求記号:

S10400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052083
シリーズID:	PA00000058
会議名:	Wichita Aviation Technology Congress & Exhibition
回次:	2008
会議開催地:	Wichita, Kansas, USA
会議開催年:	2008.08.19-2008.08.21
論文注記:	2008 Wichita Aviation Technology Congress, August, 19-21, 2008, Wichita, Kansas, USA

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1 テクニカルペーパー THE LOW FREQUENCY OSCILLATION IN THE FLOW OVER A NACA0012 AIRFOIL WITH AN LEADING EDGE Zaman, K. B.M.Q. et al. National Aeronautics and Space Administration	7 テクニカルペーパー Numerical Study of Roughness Effects on a NACA0012 Airfoil Using a New Two-Equation Closure of the Rough Wall Layer Modeling M. Lu, W. Liou American Institute of Aeronautics and Astronautics
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