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Analogue/Digital Wind Tunnel Testing of Active Low Momentum Flow Control on Single and Multi-Component Airfoil Systems at High Lift.

Author(s):
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
2002
Pub. date:
2002
Serial:
2002-0303
Paper no.:
2002-0303
Pages:
12
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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