Affiliation:
1. 206 Staff Room Rocket Force University of Engineering Xi'an 710025 China
Funder
National Natural Science Foundation of China
Subject
General Chemical Engineering,General Chemistry
Reference19 articles.
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3. Strength criterion of composite solid propellants under dynamic loading
4. A thermovisco-hyperelastic constitutive model of HTPB propellant with damage at intermediate strain rates;Wang Z.;Mech. Time-Depend. Mater.,2017
5. Compressive mechanical properties of HTPB propellant at low, intermediate, and high strain rates
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