A Flight Investigation of Exhaust-Heat De-Icing, Special Report

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The National Advisory Committee for Aeronautics has conducted exhaust-heat de-icing tests inflight t o provide data needed in the application of this method of ice prevention. Thc capacity to extract heat from the exhaust gas for de-icing purposes, the quantity of heat required, and other factors were examined. The results indicate that a wing-heating system employing a spanwise exhaust tube within the leading edge of the wing will make available for de-icing purposes between 30 and 35 percent of the exhaust-gas heat. Data are given by which the heat required for ice prevention can be calculated. Sample calculations have been made, on a basis of existing engine power over wing area ratios, to show that sufficient heating can be obtained for ice protection on modern transport airplanes,

Authors

• Rodert, Lewis A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab.
• Jones, Alun R. National Advisory Committee for Aeronautics. Langley Aeronautical Lab.