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Effect of Camber and Twist on the Stability Characteristics of Models Having a 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds
Document ID
19930087169
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
White, Maurice D
Date Acquired
August 16, 2013
Publication Date
August 29, 1952
Report/Patent Number
NACA-RM-A52F16
Report Number: NACA-RM-A52F16
Accession Number
93R16459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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