Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel

DOI10.1063/1.1572874zbMath1186.76252OpenAlexW2095020743MaRDI QIDQ3556516

D. V. Khotyanovsky, A. N. Kudryavtsev, S. B. Nikiforov, Mikhail S. Ivanov, Alexander A. Pavlov

Publication date: 22 April 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.1572874

zbMATH Keywords

hysteresisnoisereflectionshock waveswind tunnels

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (9)

Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream ⋮ Development of parallel direct simulation Monte Carlo method using a cut-cell Cartesian grid on a single graphics processor ⋮ Experiments on the mechanism of inducing transition between regular and Mach reflection ⋮ Shock transformation and hysteresis in underexpanded confined jets ⋮ Hysteresis phenomenon in supersonic flow past a system of cylinders ⋮ Effects of a single-pulse energy deposition on steady shock wave reflection ⋮ Shock reflection and oblique shock waves ⋮ Open channel flow through a linear contraction ⋮ Dynamics of unsteady asymmetric shock interactions

This page was built for publication: Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel