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Control of shock wave/turbulent boundary layer interactions using tangential injection

Author(s):
Donovan, J.F. ( McDonnell Douglas Aerospace )  
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
1996
Pub. Year:
1996
No.:
96-0443
Paper no.:
96-0443
Page(from):
1
Page(to):
22
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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