Formation mechanism and evolution of interfacial residual stress between composite propellant and rubber liner during curing process

Author:

Gao Hanjun,Tao Xinrui,Yuan Hao,Zhan Guozhu,Sun Tianmei,Zhang Xiuyan,Wen Yanwei,Wu Qiong

Publisher

Elsevier BV

Reference45 articles.

1. A variational approach for accurate prediction of stress and displacement fields and thermo-elastic constants in general symmetric laminates containing ply cracking and delamination under general triaxial loading;Hajikazemi;Int. J. Solids. Struct.,2022

2. Fluid-thermo-structural response of actively cooled scramjet combustor in hypersonic accelerating-cruise flight;Gopinath;Int. J. Heat. Mass Transf.,2022

3. Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments;Mungiguerra;Int. J. Heat. Mass Transf.,2020

4. Simulated experiment on case overheating failure of solid rocket motor under flight overload condition;Li;Appl. Therm. Eng.,2020

5. Heat transfer augmentation by recombination reactions in turbulent reacting boundary layers at elevated pressures;Perakis;Int. J. Heat. Mass Transf.,2021

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