Load Reduction Potential Using Airfoils with Variable Trailing Edge Geometry

Load Reduction Potential Using Airfoils with Variable Trailing Edge Geometry

Author(s):

Buhl, T. ( Risoe National Laboratory, Roskilde, Denmark )
Gaunaa, M.
Bak, C.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

43rd

Pub. Year:

2005

No.:

2005-1183

Paper no.:

AIAA Paper 2005-1183

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200502 [CD-ROM 2005 Disc 2]

Type:

Technical Paper

Details

TDL ID:	ZA00001617
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	43rd
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2005.01.10-2005.01.13

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