DTIC ADA041219: Computer Program for Calculation of Separated Turbulent Flows on Axisymmetric AfterbodiesReport as inadecuate



 DTIC ADA041219: Computer Program for Calculation of Separated Turbulent Flows on Axisymmetric Afterbodies


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A computer code for a turbulent boundary-layer, inviscid interaction method for axisymmetric configurations of the type used for isolated nozzle afterbody models is presented. The method is applicable to flows subsonic free streams, including slightly supercritical flows. The method consists of an integral boundary-layer method and a finite-differe

Author: Defense Technical Information Center

Source: https://archive.org/







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