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The Effects on the Aerodynamic Characteristics of Varying the Wing Thickness Ratio of a Triangular Wing-body Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method
Document ID
19930087023
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hall, Albert W
Mckay, James M
Date Acquired
August 16, 2013
Publication Date
April 2, 1952
Report/Patent Number
NACA-RM-L52B18
Accession Number
93R16313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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