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Titlebook: Interaction of Shock Waves; R. S. Srivastava Book 1994 Springer Science+Business Media Dordrecht 1994 dynamics.fluid mechanics.mechanics.s

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Introduction,last effect on supersonic aircrafts from the view point of weapon analysis and the vulnerability of either a missile or a re-entry vehicle to blast. This branch of science inspite of its manifold utility has not received the attention it warrants because of considerable difficulties involved in obtaining the solution of the problems.
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Diffraction of Normal Shock by Yawed Wedges,ity .. If an equal and opposite velocity is superimposed on the whole field, the shock becomes stationary and we have the steady flow behind the shock . The flow in fact in many respects has similarity to Busemann’s cone field problem .
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978-94-010-4474-5Springer Science+Business Media Dordrecht 1994
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Interaction of Shock Waves978-94-011-1086-0Series ISSN 0926-5112 Series E-ISSN 2215-0056
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https://doi.org/10.1007/978-94-011-1086-0dynamics; fluid mechanics; mechanics; shock wave; waves
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Fluid Mechanics and Its Applicationshttp://image.papertrans.cn/i/image/470423.jpg
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