Abstract
The present paper is a review of the work on heat addition with which the author has been concerned. It deals first with some general principles of heat addition, both at low Mach number in two dimensions and in general compressible flow in one dimension, with either constant or slowly varying cross section. A general two-dimensional method is then described with some examples of propulsion for a waverider aircraft. The special case of isothermal heat addition is discussed, and a general discussion is given of heat addition associated with separated flow, as in a flame-holder.
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