Transition between regular and Mach reflection of shock waves: New numerical and experimental results
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Publication:5950158
DOI10.1007/PL00004075zbMath0978.76514MaRDI QIDQ5950158
D. V. Khotyanovsky, V. M. Fomin, D. Vandromme, A. N. Kudryavtsev, Abdellah Hadjadj, Mikhail S. Ivanov
Publication date: 12 February 2002
Published in: Shock Waves (Search for Journal in Brave)
Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05)
Related Items (14)
Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream ⋮ A combined ghost-point-forcing / direct-forcing immersed boundary method (IBM) for compressible flow simulations ⋮ Geometric criterion for RR↔MR transition in hypersonic double-wedge flows ⋮ Streamwise vortex breakdown due to the interaction with crossed shock waves ⋮ Hysteresis phenomenon in supersonic flow past a system of cylinders ⋮ Transition between the regular and Mach shock interaction regimes initiated by a temperature disturbance ⋮ Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a \(M_\infty=9\) hypersonic flow ⋮ Effects of a single-pulse energy deposition on steady shock wave reflection ⋮ Shock reflection and oblique shock waves ⋮ Viscous simulation of shock-reflection hysteresis in overexpanded planar nozzles ⋮ Regular reflection in self-similar potential flow and the sonic criterion ⋮ Downstream flow condition effects on the RR → MR transition of asymmetric shock waves in steady flows ⋮ Convexity of self-similar transonic shocks and free boundaries for the Euler equations for potential flow ⋮ Splitting algorithms for numerical solution of Navier-Stokes equations in fluid dynamics problems
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