Physics of Plasmas · 2016 · 26 citations · 14 references
EngineeringAerospace EngineeringPhysicsComputational Fluid DynamicsFluid DynamicsMicrowave EngineeringShock CapturingShock WavesSupersonic AerodynamicsEnergy DepositionEuler EquationsMach NumberMach Number EffectsMicrowave Energy DepositionPressure DropSupersonic FlowUnsteady Flow
The article is devoted to experimental and numerical studies of the efficiency of microwave energy deposition into a supersonic flow around the blunt cylinder at different Mach numbers. Identical conditions for energy deposition have been kept in the experiments, thus allowing to evaluate the pure effect of varying Mach number on the pressure drop. Euler equations are solved numerically to model the corresponding unsteady flow compressed gas. The results of numerical simulations are compared to the data obtained from the physical experiments. It is shown that the momentum, which the body receives during interaction of the gas domain modified by microwave discharge with a shock layer before the body, increases almost linearly with rising of Mach number and the efficiency of energy deposition also rises.
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Plasmas in high speed aerodynamics
P. Bletzinger, B. N. Ganguly, David Van Wie et al. · Journal of Physics D Applied Physics · 2005 · 321 citations
Energy deposition in supersonic flows
Russell Adelgren, Gregory Elliot, Doyle Knight et al. · 39th Aerospace Sciences Meeting and Exhibit · 2001 · 86 citations