Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction

Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction

著者名:

J. Lee ( Stanford University, Stanford, CA, U.S.A. )
A. Jameson

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:

2009

発行年:

2009

通号:

2009-0897

ペーパー番号:

AIAA Paper 2009-0897

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200901

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052180
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
回次:	47th
会議開催地:	Orlando, Florida
会議開催年:	2009.01.05-2009.01.08
論文注記:	47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 5-8 January 2009, Orlando, Florida

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