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Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body combination
Document ID
19930087471
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Carmel, Melvin M
Date Acquired
August 29, 2013
Publication Date
January 27, 1953
Report/Patent Number
NACA-RM-L52L26b
Report Number: NACA-RM-L52L26b
Accession Number
93R16761
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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