- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- A method for calculating the rate of heat transfer from the surface of an airfoil or streamline body is presented. A comparison with the results of an experimental investigation indicates that the accuracy of the method is good. This method may be used to calculate the heat supply necessary for heat de-icing or in ascertaining the heat loss from the fuselage of an aircraft operating at great altitude. To illustrate the method, the total rate of heat transfer from an airfoil is calculated and compared with the experimental results.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19930091907.
Accession ID: 93R21197.
- No Copyright.
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