Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft

Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft

Author(s):

M. Martin ( Northrop Grumman Corporation, Palmdale, CA )
A. Carpenter ( Texas A&M University, College Station, TX )
W. Saric

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : U.S. Air Force T&E Days

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-1636

Paper no.:

AIAA Paper 2008-1636

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200802 [CD-ROM 2008 Disc 2]

Type:

Technical Paper

Details

TDL ID:	ZA00049520
Series ID:	PA00000047
Conf. info. (Name):	U.S. Air Force T&E Days
Conf. info. (Number):	2008
Conf. info. (Venue):	Los Angels, CA
Conf. info. (Date):	2008.02.05-2008.02.07
Note for article:	U.S. Air Force T&E Days, 5-7, February 2008, Los Angels, California

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