摘要
选择先导式减压器设计方案,进行静态特性计算。使用工程系统仿真高级建模环境(Advanced Modeling Environment for performing Simulation of engineering systems,AMESim)对静态及动态特性进行仿真分析。仿真结果表明,不同结构要素需合理设臵,以保证减压器性能满足要求。
Design program of pilot pressure reducer was chosen to complete the static feature calculation. AMESim software was used for the simulation analysis of static and dynamic features. The simulation result showed that different structure elements should be set up appropriately to guarantee the performances of pressure reducer.
出处
《导弹与航天运载技术》
北大核心
2016年第2期81-85,共5页
Missiles and Space Vehicles
