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Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds
Document ID
19930088987
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wetzel, Benton E
Date Acquired
August 16, 2013
Publication Date
November 18, 1955
Report/Patent Number
NACA-RM-A55H04a
Report Number: NACA-RM-A55H04a
Accession Number
93R18277
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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