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Lift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces
Document ID
19930088627
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gillespie, Warren, Jr
Date Acquired
August 16, 2013
Publication Date
April 25, 1955
Report/Patent Number
NACA-RM-L55B10
Report Number: NACA-RM-L55B10
Accession Number
93R17917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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