28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-6.2.3
APPLICATION OF THE FAST CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID FLOW WITH COMBUSTION
V. V. Vlasenko, A. A. Shiryaeva
TsAGI, Russian Federation
Keywords: unsteady rans, stabilization of combustion, supersonic flow
Fast technology for computation of non-stationary viscid flows is presented. It is based on explicit scheme with Fractional Time Stepping. For boundary layers, either “wall law” boundary condition or Local Dual–Time Stepping is used. Technology is applied to supersonic flow in chamber with combustion of hydrocarbon fuel in pseudoshock.
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