1986
DOI: 10.1146/annurev.fl.18.010186.000341
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Regular and Mach Reflection of Shock Waves

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Cited by 225 publications
(99 citation statements)
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“…1b). This convergence of the flow on axis generates a conical shock [63] at the longitudinal tip of the cavity (z ∼ 4 mm at 16 ns), which then re-directs the flow again. Since the plane of the conical shock is along the z-axis, the flow is symmetrically refracted along the z-axis and a collimated jet is formed.…”
Section: Electron Density Evolution With 20 T Magnetic Fieldmentioning
confidence: 99%
“…1b). This convergence of the flow on axis generates a conical shock [63] at the longitudinal tip of the cavity (z ∼ 4 mm at 16 ns), which then re-directs the flow again. Since the plane of the conical shock is along the z-axis, the flow is symmetrically refracted along the z-axis and a collimated jet is formed.…”
Section: Electron Density Evolution With 20 T Magnetic Fieldmentioning
confidence: 99%
“…As discussed above, at θ w = 45 • , a regular reflection is observed, while at θ w = 44 • , the reflection takes the form of a Mach reflection, characterised by a Mach shock travelling nearly perpendicular to the wall. A second triple-shock configuration (triple-point), also with an associated slip line, which becomes unstable due to the Kelvin-Helmholtz instability, can be found along the reflected wave and corresponds to the sub-regime of double Mach reflection [2]. This double Mach reflection has a negative reflection angle (between the triple-point path and reflected wave) [28].…”
Section: Resultsmentioning
confidence: 95%
“…The isentropic exponent γ, the geometry (angle of the wall), and the Mach number of the incident shock M i = D/c 0 uniquely define the problem; the type of reflection is subject to change with any of those variables. Thorough reviews of the shock reflection problem have been provided by Hornung [2] and Ben-Dor [1].…”
Section: Introductionmentioning
confidence: 99%
“…For the reflection of the wedge-generated shock wave in two-dimensional flows, a hypothesis based on one-dimensional treatment of the virtual stream forming downstream of the Mach stem was commonly used [12,18]. This stream is primarily subsonic; the flow in it accelerates to form a virtual throat where the flow velocity becomes sonic; the stream becomes supersonic further downstream.…”
Section: Determining the Mach Disk Positionmentioning
confidence: 99%