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Some pressure-drag effects of rounding the leading edges of hypersonic inletsPressure-drag effects of rounding leading edges of hypersonic inlets
Document ID
19640000163
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Valentine, E. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-RP-49
Report Number: NASA-RP-49
Accession Number
64N10072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DRAG
HYPERSONIC INLET
LEADING EDGE

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