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Theoretical investigation of the effects of configuration changes on the center of pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds
Document ID
19930088745
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spahr, J Richard
Date Acquired
August 16, 2013
Publication Date
September 2, 1955
Report/Patent Number
NACA-RM-A55F02
Accession Number
93R18035
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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