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Investigation of drag and static longitudinal and lateral stability characteristics of a model of a 40.4 degree swept-wing airplane at Mach numbers of 1.56 and 2.06
Document ID
19930089564
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Carmel, Melvin M
Turner, Kenneth L
Date Acquired
August 29, 2013
Publication Date
January 18, 1957
Report/Patent Number
NACA-RM-L56I17a
Report Number: NACA-RM-L56I17a
Accession Number
93R18854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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