Design of Specimen for Composite Solid Propellant Biaxial Tensile Experiment

摘要：

This paper research on the bidirectional stress and strain conditions of composite solid propellant. According to the specialty of composite solid propellant, the theoretical analysis and verifiable design of experiment were processed based on existed domestic experiment device with considering designed specimen and loading equipment, experiment conditions and other aspects factors. The specimen of composite solid propellant biaxial tensile experiment was also designed through analyzing the stress and strain field.

关键词： solid propellant biaxial tension FEM simulation

作者: CHENG Shuu LU Tingzheng CAI Guobiao DONG Chenglin

作者单位: No.2 Heavy Machine CO., LTD. Huabei.China Undamaged Examine Centre, Beijing 100085, China Beijing Un No.2 Heavy Machine CO., LTD. Huabei.China Undamaged Examine Centre, Beijing 100085, China Beijing University of Aeronautics and Astronautics, Beijing 100083, China

会议类型: 国际会议

会议名称: 2007国际推进剂、炸药、烟火技术秋季研讨会(The 2007 International Autumn Seminar on Propellants,Explosives and Pyrotechnics)

会议地点: 西安

会议语种:英文

页码: 588-591

在线出版日期: 2007-10-23（万方平台首次上网日期，不代表论文的发表时间）