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机译:
New Mexico State Univ;
NASA;
supersonic flow; shock wave boundary layer interaction; turbulent separation; axisymmetric flow; unsteady flow; large-eddy simulation; LOW-FREQUENCY UNSTEADINESS; LARGE-EDDY SIMULATION; VELOCITY FLUCTUATIONS; INDUCED SEPARATION; HIGH-ORDER; FLOW; DYNAMICS; MOTION; MODEL;
机译:Direct numerical simulation of shock wave/turbulent boundary layer interaction in a swept compression ramp at Mach 6
机译:Numerical investigation of unswept and swept turbulent shock-wave boundary layer interactions
机译:Numerical simulation of normal shock wave/turbulent boundary-layer interaction over a bump surface
机译:pressure fluctuations on the wall adjacent to a turbulent boundary layer / by mark Harrison.
机译:mach-8Boundary-Layer实验飞行物品的分析与实验验证