Thermal stresses in a finite solid-propellant grain
<p>In order to gain a fundamental understanding of actual solid propellant thermal stress problems, the geometry of the solid propellant baa been idealized as a short, circular cylinder with flat ends. It is felt that the consideration of actual curved ends would only unduly have complicated t...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/42025 http://scholar.lib.vt.edu/theses/available/etd-04122010-083524/ |