Modeling of crack initiation and growth in solid rocket propellants using macromechanics and micromechanics theories

Modeling and simulation of crack initiation and propagation in solid rocket propellant materials were conducted using both the macromechanics approach and the micro/macromechanics approach. Due to their composition, the solid rocket propellant can be construed as particle reinforced composites. The...

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Bibliographic Details
Main Author: Lee, James H.
Other Authors: Kwon, Young W.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2013
Online Access:http://hdl.handle.net/10945/32260

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