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Preliminary results from a free-flight investigation at transonic and supersonic speeds of the longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3
Document ID
19930086055
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gillis, Clarence L
Peck, Robert F
Vitale, A James
Date Acquired
August 29, 2013
Publication Date
February 14, 1950
Report/Patent Number
NACA-RM-L9K25a
Report Number: NACA-RM-L9K25a
Accession Number
93R15345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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