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Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback
Document ID
19930088583
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
D'Aiutolo, Charles T
Henning, Allen B
Date Acquired
August 16, 2013
Publication Date
April 28, 1955
Report/Patent Number
NACA-RM-L55A31
Report Number: NACA-RM-L55A31
Accession Number
93R17873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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