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Pisma v Zhurnal Tekhnicheskoi Fiziki, 2016 Volume 42, Issue 1, Pages 33–41 (Mi pjtf6546)

This article is cited in 2 papers

Boundaries of the ambiguity area upon reflection of compression shock waves

P. V. Bulat, V. V. Upyrev

St. Petersburg National Research University of Information Technologies, Mechanics and Optics

Abstract: Oblique shock waves can be reflected from hard walls, the axis, or the plane of symmetry, as well as from other counterpropagating shock waves with the formation of regular and Mach shock wave configurations. The specific form of shock wave structures is determined by the parameters of the problem: Mach number and intensity of incident shock waves. On the plane of parameters, there exists an ambiguity area in which laws of conservation admit both the regular and Mach reflection of shock waves. The boundaries of this region have been determined.

Keywords: Shock Wave, Mach Number, Technical Physic Letter, Wedge Angle, Incident Shock Wave.

Received: 22.07.2015


 English version:
Technical Physics Letters, 2016, 42:1, 15–18

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© Steklov Math. Inst. of RAS, 2024