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Free-flight Experience of the Lateral Stability Characteristics at Low Lift of a 45 Degree Swept-wing Rocket-propelled Model Equipped with a Nonlinear Yaw-rate Damper System at Mach Numbers from 0.76 to 1.73
Document ID
19930090110
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
D'Aiutolo, Charles T
Willoughby, William W
Coltrane, Lucille C
Date Acquired
August 16, 2013
Publication Date
February 8, 1957
Report/Patent Number
NACA-RM-L56L18
Report Number: NACA-RM-L56L18
Accession Number
93R19400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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