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Investigation of the pressure-and-velocity-coupled responses of solid propellants using the impedance tube techniqueNarayanaswami, Lakshmanan Lalgudi 08 1900 (has links)
No description available.
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Thermal stresses in a finite solid-propellant grain /Frohlich, Jurgen Paul, January 1962 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute, 1962. / Vita. Abstract. Includes bibliographical references (leaf 59). Also available via the Internet.
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Design and testing of a solid fuel fired combustor for gas turbinesAerts, Danny J. January 1984 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1984. / Typescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaves 120-122).
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The effects of acceleration upon the linear burning rate of solid-rocket propellantsTowson, Earl Raymond, 1938- January 1965 (has links)
No description available.
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Application of impedance tube technique in the measurement of burning solid propellant admittancesSalikuddin, Mohammed 05 1900 (has links)
No description available.
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The interaction of an electrothermal plasma with JA2 solid propellantRyan, Michael David, January 1900 (has links) (PDF)
Thesis (Ph. D.)--University of Texas at Austin, 2006. / Vita. Includes bibliographical references.
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Scientific predictability of solid rocket performance: Analyses of the processing parameters.Perez, Daniel Lizarraga. January 1992 (has links)
The objective of this dissertation is to present a computational model of the suspensions composing uncured composite solid propellant. The work examined highly concentrated suspensions of more than 50% solid volume, with attention to bimodal mixtures. Investigation of propellant processing was conducted to determine how this model can be applied to processing. Experimental work was conducted to supply data for comparison to the computational results. This involved data gathered from an orifice viscometer on viscosity and flow behavior. This model is a tool to investigate goodness of mixing throughout the processing stages of the propellant. The investigation into processing focused both on mixing and casting of the suspension. By studying this model for concentration, velocity and thermal behaviors, a better understanding of how well the propellant composition progresses in processing was obtained. A multiphase mixture approach was taken. This involved a continuum description for the mixture and each constituent. A Fortran program was written to construct this routine. It was run on both a VAXstation 3100, Model 40 using VMS Digital operating system, and a SUN IPX, using SUN UNIX operating system. The code examined two-dimensional monomodal and bimodel mixture flows through a pipe. It examined concentrations between 65% and 75%. Due to the high concentration, it was necessary to apply all inertial and viscous terms within each constituent and the entire mixture. Proper boundary conditions and initial conditions to produce stable runs were found. Both monomodal and bimodal computational results showed good correlations with the experimental data, although a slight dilatation was produced by the program. No dilatation appeared in the experimental work. No concentration drop was detected in either the computational results or experimental work.
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The interaction of an electrothermal plasma with JA2 solid propellantRyan, Michael David 28 August 2008 (has links)
Not available / text
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A method for determining the thermal diffusivity of solid propellant rocket fuelsSpurlock, Jack M. (Jack Marion) 08 1900 (has links)
No description available.
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Behavior of aluminum on the burning surface of a solid propellantSambamurthi, Jayaraman Kalambur 05 1900 (has links)
No description available.
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