Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel State Control

Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel State Control

Author(s):

Zink, S. ( Lockheed Martin Aeronautics Company, Ft.Worth, TX )
Love, M.
Youngren, H. ( AeroCraft Consulting, Portland, ME )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Multidisciplinary Analysis and Optimization Conference

Ser. no.:

10th

Pub. Year:

2004

No.:

2004-4365

Paper no.:

AIAA Paper 2004-4365

Pub. info.:

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

ISSN:

10877215

Language:

English

Call no.:

A07400/200417 [CD-ROM 2004 Disc 17]

Type:

Technical Paper

Details

TDL ID:	ZA00001557
Series ID:	PA00000051
Conf. info. (Name):	AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Conf. info. (Number):	10th
Conf. info. (Venue):	Albany, New York
Conf. info. (Date):	2004.08.30-2004.09.01

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