Summarization on Solid Rocket Motor Ignition Transient Fluid-Structure Interaction
The Fluid-Structure Interactions (FSI) phenomenon at Solid Rocket Motor (SRM) ignition transient was taken much more attention with the first prequalification motor (PQM-1) of Titan IV SRM exploded during its first full-scale static firing test. In this paper, research actuality and development trend of FSI which are from three parts-ignition gas flow, grain deformation and experiment are summarized at home and abroad. Combined with our national development conditions, the new approach on studying coupled Fluid-Structure at SRM ignition transient are discussed preliminarily.
solidrocketmotor ignition transient fluid-structure interactions research actuality
Qi Cao Jinxian Li Xiaona Li
College of Astronautics Northwestern Polytechnical UniversityXian, China The First Aircraft In stitute Aviation Industry Corporation of ChinaXian, China
国际会议
2011 International Conference on System Modeling and Optimization(ICSMO 2011)(2011年系统建模与优化国际会议)
贵阳
英文
80-84
2011-01-26(万方平台首次上网日期,不代表论文的发表时间)