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

Author(s):

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

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-0897

Paper no.:

AIAA Paper 2009-0897

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200901

Type:

Technical Paper

Details

TDL ID:	ZA00052180
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
Conf. info. (Number):	47th
Conf. info. (Venue):	Orlando, Florida
Conf. info. (Date):	2009.01.05-2009.01.08
Note for article:	47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 5-8 January 2009, Orlando, Florida

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