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Last edited by
RenameBot
September 13, 2008 |
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Harold William Davidson
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Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps.
by
Harold William Davidson
First published in 1951
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1 edition
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Subjects
Aerofoils
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Boundary layer
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Lift (Aerodynamics)
,
Trailing edge flaps
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ID Numbers
OLID: OL2278075A
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