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Free-flight Measurements of Some Effects of Aileron Span, Chord, and Deflection and of Wing Flexibility on the Rolling Effectiveness of Ailerons on Sweptback Wings at Mach Numbers Between 0.8 and 1.6
Document ID
19930087886
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strass, H Kurt
Fields, E M
Schult, Eugene D
Date Acquired
August 16, 2013
Publication Date
January 24, 1952
Report/Patent Number
NACA-RM-L51K16
Report Number: NACA-RM-L51K16
Accession Number
93R17176
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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