عنوان مقاله [English]
نویسندگان [English]چکیده [English]
In this study, the steady, viscous and compressible boundary-layer flow with mass transfer (suction or injection flow) over axisymmetric bodies has been numerically simulated. For this reason, a computer program has been developed that uses an implicit finite difference method to solve non-similar, full compressible boundary layer equations for calculating the distribution of heat transfer and boundary-layer characteristics over nose of bodies in supersonic flow. The numerical results for three wall-mass transfer boundary conditions; solid wall ; porous walls with suction or injection are presented. The results were compared with the available solutions in the technical literature and also with the results of implementing fluent software showing reasonable agreements.
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