Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined-Wing Aircraft

Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined-Wing Aircraft

Author(s):

V. Bond ( Air Force Institute of Technology, Wright Patterson Air Force Base, OH )
R. Canfield
M. Madruga Santos Matos ( Academia da Forca Aérea, Sintra, Portugal )
A. Suleman ( University of Victoria, Victoria, Canada )
M. Blair ( U.S. Air Force, Wright Patterson Air Force Base, OH )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-1772

Paper no.:

AIAA Paper 2007-1772

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200708 [CD-ROM 2007 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00049496
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	48th
Conf. info. (Venue):	Honolulu, Hawaii
Conf. info. (Date):	2007.04.23-2007.04.26

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