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On slender-body theory and the area rule at transonic speedsThe basic ideas of the slender-body approximation have been applied to the nonlinear transonic-flow equation for the velocity potential in order to obtain some of the essential features of slender-body theory at transonic speeds. The results of the investigation are presented from a unified point of view which demonstrates the similarity of slender-body solutions in the various Mach number ranges. The transonic area rule and some conditions concerning its validity follow from the analysis.
Document ID
19930084626
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Harder, Keith C
Klunker, E B
Date Acquired
August 16, 2013
Publication Date
November 1, 1956
Report/Patent Number
NACA-TN-3815
Report Number: NACA-TN-3815
Accession Number
93R13916
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW, SUPERSONIC
FLOW, MIXED
FLOW, SUBSONIC
WING-FUSELAGE COMBINATIONS - AIRPLANES
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