1961The Physics of FluidsRequires access

Shock-Wave Curvature at Low Initial Pressure

Russell E. Duff, James L. Young

Open publisher page 16 citations

Abstract

The shape of the primary shock wave in a shock tube has been measured by recording the time of arrival of the shock in argon at an array of piezoelectric detectors located along a diameter of a 28.6-mm i.d. shock tube operated at an initial expansion chamber pressure of 0.34 mm Hg. The following conclusions were drawn from the results: (1) Shock-wave tilt was negligibly small under the conditions of these experiments; (2) shock-wave curvature is independent of shock strength for shock Mach numbers from 1.8 to 6.3; (3) the shock-front shape is nearly spherical; (4) the axial extent or the bulge of the curved shock is approximately 1 mm. The axial extent of a shock in argon was also measured over the range of initial pressure from 0.1 to 20 mm Hg. It varies approximately as the inverse square root of the initial pressure.

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What this paper is about

The shape of the primary shock wave in a shock tube has been measured by recording the time of arrival of the shock in argon at an array of piezoelectric detectors located along a diameter of a 28.6-mm i.d. shock tube operated at an initial expansion chamber pressure of 0.34 mm Hg. The following conclusions were drawn from the results: (1) Shock-wave tilt was negligibly small under the conditions of these experiments; (2) shock-wave curvature is independent of shock strength for shock Mach numbers from 1.8 to 6.3; (3) the shock-front shape is nearly spherical; (4) the axial extent or the bulge of the curved shock is approximately 1 mm. The axial extent of a shock in argon was also measured over the range of initial pressure from 0.1 to 20 mm Hg. It varies approximately as the inverse square root of the initial pressure.

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Available abstract

The shape of the primary shock wave in a shock tube has been measured by recording the time of arrival of the shock in argon at an array of piezoelectric detectors located along a diameter of a 28.6-mm i.d. shock tube operated at an initial expansion chamber pressure of 0.34 mm Hg. The following conclusions were drawn from the results: (1) Shock-wave tilt was negligibly small under the conditions of these experiments; (2) shock-wave curvature is independent of shock strength for shock Mach numbers from 1.8 to 6.3; (3) the shock-front shape is nearly spherical; (4) the axial extent or the bulge of the curved shock is approximately 1 mm. The axial extent of a shock in argon was also measured over the range of initial pressure from 0.1 to 20 mm Hg. It varies approximately as the inverse square root of the initial pressure.

Key concepts: Physics, Oblique shock, Moving shock, Shock tube, Shock wave, Shock (circulatory), Mach number, Mechanics

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