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Generalized conical-flow fields in supersonic wing theory
Document ID
19930083213
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lomax, Harvard
Heaslet, Max A
Date Acquired
August 16, 2013
Publication Date
September 1, 1951
Report/Patent Number
NACA-TN-2497
Report Number: NACA-TN-2497
Accession Number
93R12503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, COMPLETE - SWEEP
FLOW, SUPERSONIC
WINGS, COMPLETE - THEORY
LOADS, STEADY - WINGS
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