Numerical and analytical study of transverse supersonic flow over a flat cone |
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| Authors: | D L Book S Eidelman I Lottati X Yang |
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| Institution: | (1) Code 4405, Naval Research Laboratory, 20375 Washington, DC;(2) Science Applications International, 22102 McLean, VA |
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| Abstract: | Quasisteady supersonic flow over a flat cone on a plane surface is studied. A formula is derived for the angle through which the flow lines turn at the cone. The results are used to justify the use of two-dimensional simulations of the flow. Peak pressures and total impulses are obtained numerically for various cone angles.This article was processed using Springer-Verlag TEX Shock Waves macro package 1990. |
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| Keywords: | Cone Euler equation Mach reflection CFD Supersonic flow |
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