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Universal behaviour in erosive burning of solid propellants

Mukunda, HS and Paul, PJ (1997) Universal behaviour in erosive burning of solid propellants. In: Combustion and Flame, 109 (1-2). pp. 224-236.

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Official URL: http://dx.doi.org/10.1016/S0010-2180(96)00150-2

Abstract

This paper considers the extensive data and correlations on the erosive burning of solid propellants. A relatively simple nondimensional relationship between the ratio of the actual to nonerosive burn rate (eta) and a quantity g, which is the product of g(0)-the ratio of free stream mass flux to the mass flux from the surface for nonerosive condition-and Re-0(m), where Re-0 is the Reynolds number based on the nonerosive mass flux of the propellant and port diameter, is shown to correlate most data within the accuracies of the experiments with m = -0.125. This shows the above relationship to account for the effects of pressure, aluminum, even up to a proportion of 17%, burn rate catalysts, and motor size. It is concluded that the suggested correlation between eta and g may be adopted universally for most practical propellants. (C) 1997 by The Combustion Institute.

Item Type: Journal Article
Additional Information: Copyright of this article belongs to Elsevier Science.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 22 Jun 2011 06:30
Last Modified: 22 Jun 2011 06:30
URI: http://eprints.iisc.ernet.in/id/eprint/38558

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