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Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
Document ID
19930088565
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Platt, Robert J , Jr
Brooks, Joseph D
Date Acquired
August 29, 2013
Publication Date
April 4, 1955
Report/Patent Number
NACA-RM-L54L31b
Report Number: NACA-RM-L54L31b
Accession Number
93R17855
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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