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Static Longitudinal Stability and Control Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Document ID
19930088584
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Driver, Cornelius
Foster, Gerald V
Date Acquired
August 16, 2013
Publication Date
July 11, 1956
Report/Patent Number
NACA-RM-L56D04
Report Number: NACA-RM-L56D04
Accession Number
93R17874
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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