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A method for determining the rate of heat transfer from a wing or streamline body
Document ID
19930093519
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mccullough, George B
Date Acquired
September 6, 2013
Publication Date
December 1, 1942
Report/Patent Number
NACA-WR-A-40
Report Number: NACA-WR-A-40
Accession Number
93R22809
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW - COMPRESSIBILITY
THEORIES - HEAT TRANSMISSION
HEAT TRANSMISSION - PLATES, FLAT
ICE PREVENTION - HEATING
BOUNDARY LAYER - AIRFOILS
ICE PREVENTION - WINGS
HEAT TRANSMISSION - STREAMLINE BODIES
WIND TUNNEL TESTS - AAL (10' X 7') WORK CARRIED OUT AT AAL
HEAT TRANSMISSION - AIRFOILS

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