Author:
Zhou Qingchun,Xu Jinsheng,Chen Xiong,Zheng Jian,Zhou Changsheng
Funder
Natural Science Foundation of Jiangsu Province
Nanjing University of Science & Technology
Subject
Polymers and Plastics,General Chemical Engineering,Biomaterials
Reference25 articles.
1. Cohesive zone modeling of propellant and insulation interface debonding;Zhou;J Adhes,2014
2. Investigation of the fracture mechanism and fracture energy of HTPB propellant/liner interface debonding;Zhou;Acta Armamentarii,2014
3. Bonding of composite propellant in cast-in-case rocket motors;Gustavson;J Spacecr Rockets,1966
4. Christiansen AG, Laheru KP, Anderson GP. Cohesive and adhesive analog test specimens for solid propellant grain simulation. In: Proceedings of the AIAA, SAE, and ASME, joint propulsion conference, 19th, Seattle, WA; 1983:27(29).
5. Kuhlmann T, Peeters R, Bills K. Modified maximum principal stress failure criterion applied to propellant-liner bond failures. In: Proceedings of the AIAA, SAE, ASME, and ASEE, joint propulsion conference, 21st, Monterey, CA; 1985:8(10).
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