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Dynamic Directional Stability Derivatives for A 45 Degree Swept-Wing-Vertical-Tail Airplane Model at Transonic Speeds and Angles of Attack, With A Description of the Mechanism and Instrumentation Employed
Document ID
19930090056
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Albert L. Braslow (Langley Memorial Aeronautical Laboratory Hampton, United States)
Harleth G. Wiley (Langley Memorial Aeronautical Laboratory Hampton, United States)
Cullen Q. Lee (Langley Memorial Aeronautical Laboratory Hampton, United States)
Date Acquired
August 29, 2013
Publication Date
April 21, 1958
Report/Patent Number
NACA-RM-L58A28
Accession Number
93R19346
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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