Determining chordwise distribution of rate of heat transfer from surface of wing or body of revolution to air with view to ice prevention on aircraft; comparison of calculated average heat transfer coefficient for nose section of wing of Lockheed 12-A airplane with that experimentally determined shows satisfactory agreement. (25¢)
Method for calculating heat transfer in laminar flow region of bodies
Nat Advisory Committee Aeronautics -- Report
1947
Bibliography
Report
Englisch
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