NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Contribution to the theory of the heated duct radiatorA method is developed with no neglect of certain factors in mass flow of air and in the drag of the heated radiator, i.e., one under actual operating conditions, as compared with the corresponding values in the cold state, may be simply computed. Although a symmetrical duct radiator has been used to bring out the flow relations, the results apply equally as well to the unsymmetrical radiator shapes usual in airplane construction.
Document ID
19930094523
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Winter, H
Date Acquired
September 6, 2013
Publication Date
April 1, 1939
Report/Patent Number
NACA-TM-893
Report Number: NACA-TM-893
Accession Number
93R23443
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available