Methods for calculating unit thermal conductance on outer surface of heated wing involving both laminar and turbulent boundary layers; new equation suggested should indicate effect of pressure gradient on laminar heat transfer to greater degree than heretofore; different equations applied to Joukowski profile.
Investigation of aircraft heaters XXIX -- Comparison of several methods of calculating heat losses from airfoils
Nat Advisory Committee Aeronautics -- Tech Note
1948
70 pages
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English
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