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Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections
Document ID
19930086810
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strass, H Kurt
Fields, E M
Schult, Eugene D
Date Acquired
August 16, 2013
Publication Date
June 22, 1951
Report/Patent Number
NACA-RM-L51D18a
Report Number: NACA-RM-L51D18a
Accession Number
93R16100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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