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Numerical Study of Shockwave Induced Boundary Layer Separation Control using Plasma Actuators

Author(s):
Publication title:
AIAA meeting papers on disc
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
2008
Pub. Year:
2008
No.:
2008-1095
Paper no.:
AIAA Paper 2008-1095
Pub. info.:
Reston, Va.: American Institute of Aeronautics and Astronautics
ISSN:
10877215
Language:
English
Call no.:
A07400/200801 [CD-ROM 2008 Disc 1]
Type:
Technical Paper

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