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AN ANALOG STUDY OF THE INFLUENCE OF INTERNAL MODIFICATIONS TO A WING LEADING EDGE ON ITS TRANSIENT TEMPERATURE RISE DURING HIGHSPEED FLIGHTAerodynamic heating of sweptback wing leading edge
Document ID
19630004001
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Neel, C. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 1, 2013
Publication Date
March 17, 1958
Subject Category
Geophysics
Report/Patent Number
NACA-RM-A57K21
Report Number: NACA-RM-A57K21
Accession Number
63N13877
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPTBACK WING
LEADING EDGE
AERODYNAMIC HEATING

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