摘要
本文提出了可实现预期内弹道的气动式水下发射器发射阀仿真设计方法 ,建立了发射阀仿真设计的三个基本模型 :内弹道、发射阀开启面积变化规律计算和发射阀设计模型。运用该方法进行了发射阀特形孔的实例仿真设计 ,证明了设计方法的可行性 。
A method for the simulated design of launching valve for the compressed air launcher was put forward, that can attain the designed trajectory. Three mathematical models including interior trajectory model, launching valve opening area calculation model and launching valve design model were established. The method and mathematical models have been tested on the simulation design of the shape of the aperture with a launching valve, and proved its availability for the optimal design of the launching valve.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2003年第3期354-358,共5页
Acta Armamentarii
