Abstract
K of the subsonic flowfield in the vicinity of air inlets or wedges is a necessity for engineering design and analysis. This Note presents the results of numerical solutions for two-dimensional subsonic compressible flows. In order to obtain a solution it is necessary to introduce several severe restraints such as field representation, field boundaries, and body surface configuration changes. The effects of these restraints have been investigated and the optimum methods are presented. Emmons, Amick, and other investigators' have treated the various methods of solution of the simultaneous difference equations that represent the continuous flowfield in terms of a discretized flowfield. Fox has presented some methods for representing the discontinuous finite slope changes of bound-
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