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NUMERICAL RESEARCH OF THE FLOW OVER A SUPERSONIC AIRCRAFT WITH A TRANSVERSE GAS JET

Volume 43, Edição 6, 2012, pp. 737-751
DOI: 10.1615/TsAGISciJ.2013007324
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RESUMO

The results of numerical research on the aerodynamics characteristics of a supersonic aircraft model with a transverse gas jet are introduced in this article. The research was done with and without a transverse gas jet. The main purpose of this research was to find the aerodynamics coefficients of the forces and moments produced by the interaction of the gas jet and free-stream flow. The jet pipes were placed near the center of mass. The results for transonic and supersonic flights are compared.

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