Evolution of weak shock wave in two-dimensional steady supersonic flow in dusty gas

dc.contributor.author	Chaturvedi R.K.; Gupta P.; Singh L.P.
dc.date.accessioned	2025-05-24T09:40:01Z
dc.description.abstract	The present paper concerns with the propagation of weak shock waves in a dusty gas governed by the quasilinear hyperbolic partial differential equations. Using the method of wavefront analysis the transport equations governing the evolution of weak discontinuities are derived. Transport equations are used to determine the shock formation distance and conditions which ensure that there will not evolve any shock. Also the influence of dust particles, ratio of specific heats and upstream flow Mach number on the shock formation distance is analyzed. © 2019 IAA
dc.identifier.doi	https://doi.org/10.1016/j.actaastro.2019.02.021
dc.identifier.uri	http://172.23.0.11:4000/handle/123456789/18735
dc.relation.ispartofseries	Acta Astronautica
dc.title	Evolution of weak shock wave in two-dimensional steady supersonic flow in dusty gas

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