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Some considerations regarding the application of the supersonic area rule to the design of airplane fuselagesSupersonic aircraft fuselage design for minimum wave drag
Document ID
19660024790
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Whitcomb, R. T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 3, 1956
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L56E23A
Report Number: NACA-RM-L56E23A
Accession Number
66N34080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC AIRCRAFT
AIRCRAFT DESIGN
FUSELAGE
WAVE DRAG

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