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Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration having a 60 degree delta wing and a high unswept horizontal tail
Document ID
19930087370
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Peck, Robert F
Mitchell, Jesse L
Date Acquired
August 29, 2013
Publication Date
January 5, 1953
Report/Patent Number
NACA-RM-L52K04a
Report Number: NACA-RM-L52K04a
Accession Number
93R16660
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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