The phenomenon of shock wave reflection was first reported by the distinguished. The edge of the cone forms a supersonic wave front with an unusually large amplitude called a shock wave. Study on mach reflection and mach configuration cscamm. Queens university mech 448 chapter fivechapter five. Triple point point of intersection of the incident, mach and reflected shocks. Examples of shock wave reflection from multiple wedges and curved wedges are. Focusing of a toroidal shock wave emitted from a coaxial annular shock tube and the resulting shock wave reflection were studied numerically with a dispersioncontrolled scheme. Shock wave reflection phenomena gabi bendor springer. Shock wave reflection phenomena request pdf researchgate.
Aerospace free fulltext shock wave diffraction phenomena. The graphic at the top shows the wedges in red and green and the shock wave generated by the wedge as a line. Pdf while a moving incident shock wave moves through a sharp compression ramp. Shock waves in gas dynamics 61 courantfriedrichss book 19 gives the account of the e. A schematic of the experimental configuration is shown in fig. This book presents a wealth of images of shock wave phenomena, gathered by the author over the past 40 years. The aim of this study is to show the evidence of mach stem formation for very weak shock waves with acoustic mach numbers on the order of 10. This exponential variation of the incident shock wave pressure is accurate for at least about one decay constant. The phenomenon of shock wave reflection was first reported by the distinguished philosopher ernst mach in 1878. Furthermore, combining with appropriate local non isotropic rescaling to. Much has been learnt about the existence of shock waves over the years, but little is known about its interactions with other fluid dynamic processes. Steady, pseudosteady and unsteady shock wave reflections. In the present study, the reflection phenomena of the shock waves have been investigated experimentally over a wide range of incident shock mach numbers and wedge angles using air or chlorofluorocarbon freon12, as a working gas. Monte carlo analysis of the hysteresis phenomenon in.
A random type disturbance is 120 feet below the surface. Interaction of an oblique shock wave with a pair of parallel. The interaction of a shock wave and a vortex pair is more complicated than that of a shock wave and a single vortex. Moreover, since the changes across the oblique shock wave are no longer small, this feature of the. This surface at which the pressure and also density and velocity change discontinuously is called a shock wave. Shock wave reflection is one of the most important fluid dynamic processes, which has been investigated rigorously.
Free boundary problems in shock reflectiondiffraction and related transonic. Ernst mach was the first scientist who experimentally observed the phenomenon of shock wave reflection. When a shock wave, which is moving with a constant velocity, propagates over a solid wedge, the flow generated by the shock impinges on the wedge thus generating a second reflected shock, which ensures that the velocity of the flow is parallel to the wedge surface. Shock wave reflection phenomena springer for research. Like an ordinary wave, a shock wave carries energy and can propagate through a medium but is characterized by an abrupt, nearly discontinuous, change in pressure, temperature, and density of the medium. In the field of aerospace engineering, the study of the characteristics of vortical flows and their unsteady phenomena finds numerous engineering applications related to improvements in the design of tip devices, enhancement of combustor performance, and control of noise generation. In this paper the local change of the mach stem curvature was experimentally and numerically investigated. Reflection and focusing of toroidal shock waves from coaxial. It contains more complicated physical phenomena including shock wave distortion. Raizer academy of sciences, moscow edited by wallace d.
When a weak shock wave reflects from wedges its reflection pattern does not appear to be a simple mach reflection. Experimental investigations oil the reflection of plane shock waves over straight wedges indicated that there is a domain, the weak shock wave domain, inside which the resulted wave configurations. Investigating shock waveboundary layer interaction caused by. The line is colored blue for an oblique shock and magenta when the shock is a normal shock. Transition boundary between regular and mach reflections. The numerical code was first applied to prediction of a shock wave discharged from the openend of a circular shock tube into ambient air. Shock reflection is a fundamental phenomenon in studying compressible flow. When a shock wave reaches an observer a sonic boom is heard. When relaxation phenomena are present, a shock wave actually reflects with a speed which varies during the time required for the reflected shock wave to travel through the nonuniform relaxation zone behind the incident shock wave. In physics, a shock wave also spelled shockwave, or shock, is a type of propagating disturbance that moves faster than the local speed of sound in the medium.
However, the introduction of new lithotripters appears to have increased the potential problems of shock wave application compared with firstgeneration devices 4,5. Understanding these shock reflectiondiffraction phenomena requires a. A weak shock wave reflection over wedges springerlink. Furthermore, combining with appropriate local nonisotropic rescaling to. A basic feature of hyperbolic systems of conservation laws is that there are rich phenomena of wave interactions involving shock waves and contact discontinuities. Mech 448 a photograph of a normal shock wave is shown in the following figure. However, in regard to these reflections, there are many questions which are not yet resolved. Various shock wave focusing apparatus that have been tested are described, including a detonation chamber, a setup for focusing weak blast waves and a configuration for obtaining timestepped shadowgraphs of converging cylindrical shocks. Shock waves an international journal on shock waves. Stateoftheart in research on mach reflection of shock waves. A large amount of work has been carried out in the analysis of the shock wave diffraction around conventional. The course is planned based mainly on this book and. The explosively driven shock tube is used to produce a relevant laboratory size blast wave.
Nonuniqueness of solutions in asymptotically selfsimilar shock. The performance ofa reflected shock tunnel according to perfectgas theory. The reflection of a steadily moving shock wave on a. Free boundary problems in shock reflectiondiffraction and related.
Oblique shockwave reflections are analyzed by means of. Apr 06, 2018 the flow variables are presented as ratios to the previous zone up and to the free stream value 0. Download it once and read it on your kindle device, pc, phones or tablets. Mach stem formation in reflection and focusing of weak shock. Shock wave reflection phenomena shock wave and high pressure. Physics of shock waves and hightemperature hydrodynamic. Regular and mach reflection of shock waves1 hans hornun9 institute for experimental fluid mechanics, dfvlr, bunsenstrabe 10, d3400 grttingen, federal republic of germany introduction the properties that distinguish a shock wave from other waves are that its thickness is negligible compared with other characteristic lengths, and that. Wave phenomena reflection of waves index information about this applet related applets. Pdf study on the mach and regular reflections of shock wave. The first part is a thorough introduction to oblique shock wave reflections. Numerical investigations on blast wave attenuation by obstacles.
Mech 448 a shock wave is extremely thin, the shock wave normally only being a few mean free paths thick. Ernst mach has been dubbed the fist scientist to notice and record the reflection phenomena of shock waves. Thiscausticstructure isanoblique shock wave and when the. Mach reflection can exist in steady, pseudosteady and unsteady flows. The first part is a thorough introduction to oblique shock wave reflections, presenting the two major wellknown reflection wave configurations. Shock wave re ection phenomena, springer, new york, 1992. Assuming perfectgas behaviour, and that the ratio of specific heats, 7, is the same for the driver and driven gases, the equations given below determine the motion of the shocks and contact surface, and the. This book provides a comprehensive stateoftheknowledge description of the shock wave reflection phenomena from a phenomenological point of view. The changes that occur through a normal shock wave, i. Use features like bookmarks, note taking and highlighting while reading shock wave reflection phenomena shock wave and high pressure phenomena.
Highly resolved, twodimensional numerical simulations of compressible viscous flow demonstrate the bifurcation of the reflecting shock wave from the reflection of an ideal detonation. Hysteresis processes in the regular reflection mach reflection transition in steady flows progress in aerospace sciences, vol. After that point, the incident shock wave pressure actually begins to decay at a slower rate in the tail of the shock wave. Research works in this field were collected and compiled nicely in the famous book shock wave reflection phenomena by prof. The first part is a thorough introduction to oblique shock wave reflections, presenting the two major wellknown reflection wave configurations, namely, regular rr and mach mr reflections, the corresponding two and three shock theories, their analytical and graphical solution and the proposed transition boundaries between these two.
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