Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration

Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration

Author(s):

T. Skujins ( University of Michigan, Ann Arbor, MI )
C. Cesnik
M. Oppenheimer ( Air Force Research Laboratory, Dayton, OH )
D. Doman

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-6384

Paper no.:

AIAA 2008-6384

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200810 [CD-ROM 2008 Disc 10]

Type:

Technical Paper

Details

TDL ID:	ZA00050905
Series ID:	PA00000162
Conf. info. (Name):	AIAA Atmospheric Flight Mechanics Conference and Exhibit
Conf. info. (Number):	2008
Conf. info. (Venue):	Honolulu, HI
Conf. info. (Date):	2008.08.18-2008.08.21

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