An investigation of aircraft heaters 36: preliminary investigation of a combustion-type aircraft heater
Description: Report presenting experimental results on the thermal performance of an aircraft combustion-type heater. The performance of the heater with a counterflow and a parallel-flow return passage on the gas side does not appear predictable by use of existing equations. The thermal conductance for the gases within the combustion chamber is predicted to be many times lower than the experimental data indicate.
Date: August 1951
Creator: Boelter, Llewellyn Michael Kraus; Elswick, W. R.; Sanders, V. D. & Rubesin, M. W.
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Partner: UNT Libraries Government Documents Department