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The Use of Source-sink and Doublet Distributions Extended to the Solution of Boundary Value Problems in Supersonic Flow
Document ID
19930082200
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Heaslet, Max A
Lomax, Harvard
Date Acquired
August 16, 2013
Publication Date
January 1, 1948
Report/Patent Number
NACA-TN-1515
Report Number: NACA-TN-1515
Accession Number
93R11490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION - WINGS, DELTA
EQUATIONS - FLOW - DOUBLETS
THEORIES - FLOW - SUPERSONIC
MATHEMATICS - BOUNDARY VALUE
MATHEMATICS - INTEGRALS
EQUATIONS - FLOW - SOURCES & SINKS
ROLLING & PITCHING MOMENTS - WINGS, DELTA
THEORIES - WINGS - SUPERSONIC
LOAD DISTRIBUTION - WINGS
THEORIES - AIRFOILS - THIN

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