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As an important component, the nozzle produces most of thrust in scramjets. A new concept of increasing the aerodynamics of the scramjet nozzle with energy addition is presented. The essence of the method is to create a heated region in the inner flow field of the scramjet nozzle. In this paper, the two-dimensional coupled implicit compressible Reynolds Averaged Navier–Stokes (RANS) and Menter's shear...
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