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Aerodynamic Load Distribution over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03
Document ID
19930090075
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
West, F E , Jr
Whitcomb, Charles F
Schmeer, James W
Date Acquired
August 16, 2013
Publication Date
December 5, 1957
Report/Patent Number
NACA-RM-L57J11
Report Number: NACA-RM-L57J11
Accession Number
93R19365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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