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JOURNALS // Fizika Goreniya i Vzryva // Archive

Fizika Goreniya i Vzryva, 2011 Volume 47, Issue 2, Pages 74–80 (Mi fgv1085)

This article is cited in 7 papers

Experimental study of the acoustic admittance of the burning surface of composite solid propellants

V. A. Arkhipova, S. A. Volkovb, L. N. Revyaginb

a Institute of Applied Mathematics and Mechanics, Tomsk State University, Tomsk, 634050, Russia
b Tomsk State University, Tomsk, 634050, Russia

Abstract: A method for measuring the acoustic admittance of the burning surface of solid propellants using a two-dimensional combustion chamber (T-burner) is considered. The paper presents the results of an experimental study of the effect of the pressure and frequency of acoustic oscillations in the combustion chamber and the effects of the composition, mass content, and aluminum powder particle size on the acoustic admittance of the burning surface of composite solid propellants.

Keywords: composite solid propellant, aluminum powder, burning surface, T-burner, acoustic admittance.

UDC: 629.194.632.1:536.46

Received: 10.02.2010
Accepted: 30.03.2010


 English version:
Combustion, Explosion and Shock Waves, 2011, 47:2, 193–199

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