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Boundary layer removal by suctionFlight-test data and wind-tunnel data on suction profiles are substantially in agreement. The lift values found in the model test can be actually flown and used as a basis for the design. To visualize the action of the suction, the flow conditions with and without suction on the upper surface were photographed; figures 12 to 15 are sections of the film.
Document ID
19930094442
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schrenk, O
Date Acquired
September 6, 2013
Publication Date
April 1, 1941
Report/Patent Number
NACA-TM-974
Report Number: NACA-TM-974
Accession Number
93R23362
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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