固体火箭技术2012，Vol.35Issue(3)：348-351,4.
配合间隙对同轴线对开双喷管结构轨控发动机性能的影响
Effects of clearance on properties of orbit-control motor with double opposite nozzle
孙立刚 1李林 1邓哲 1李佳明 1张铎1
作者信息
摘要
Abstract
Different flow fields of the orbit-control motor with double opposite nozzle in different condition or in different fit clearances were numerically simulated and effect of fit clearances on orbit-control motor performance parameters was detected. Results show that when the clearance between motor and control chamber gets closer,total pressure of thrust chamber is higher;mass flow rate is lower and thrust of orbit-control motor is improved.关键词
轨控发动机/转子/配合间隙/数值仿真Key words
orbit-control motor/rotor/fit clearance/numerical simulation分类
航空航天引用本文复制引用
孙立刚,李林,邓哲,李佳明,张铎..配合间隙对同轴线对开双喷管结构轨控发动机性能的影响[J].固体火箭技术,2012,35(3):348-351,4.
