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Rocket-model Investigation to Determine the Hinge-moment and Normal-force Properties of a Full-span, Constant-chord, Partially Balanced Trailing-edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Document ID
19930089114
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Martz, C William
Goslee, John W
Date Acquired
September 6, 2013
Publication Date
October 30, 1953
Report/Patent Number
NACA-RM-L53I04
Accession Number
93R18404
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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