Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV

Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV

Author(s):

Q. Liu ( School of Aeronautics, Northwestern Polytechnical University, Xi'an, China (prc) )
J. Li
Z. Zhou ( UAV Research and Development Center, Northwestern Polytechnical University, Xi'an, China (prc) )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-3462

Paper no.:

AIAA Paper 2006-3462

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200610 [CD-ROM 2006 Disc 10]

Type:

Technical Paper

Details

TDL ID:	ZA00047231
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	24th
Conf. info. (Venue):	San Francisco, California
Conf. info. (Date):	2006.06.05-2006.06.08

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