Burning surfaces evolution in solid propellants: a numerical model

A methodology for the solution of the internal physics of solid propellant rocket motors is described. The problem involves the simulation of a burning surface - a dynamically changing interface between the solid propellant and combustion gas phases. Burning surfaces can have complex shapes that cha...

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Bibliographic Details

Main Authors:	Joanna Szmelter, P. Ortiz
Format:	Default Article
Published:	2007
Subjects:	Mechanical engineering not elsewhere classified Evolving surfaces Propulsion Unstructured meshes Mechanical Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/4693
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