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Experiments with a wing from which the boundary layer is removed by suctionThis report presents the results of the first investigation of the physical principle of preventing the streamline separation by removing the boundary layer. It was aeronautical, in that it dealt with airfoils, but the results are of a very general application.
Document ID
19930094782
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schrenk, Oskar
Date Acquired
September 6, 2013
Publication Date
August 1, 1931
Report/Patent Number
NACA-TM-634
Report Number: NACA-TM-634
Accession Number
93R23702
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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