燃烧消耗量
Modeling and Simulation of Pasty Propellant Flow in Hot Pipe
膏体推进剂在热管道内流动的建模与仿真
To know more altitude compensation and base characteristics of plug nozzle, cold-flow tests on 1-cell 2D linear plug nozzle, which utilize high pressure air as propellant were conducted.
为研究塞式喷管的高度特性和底部特性,采用高压空气为工作介质对单元直排塞式喷管进行实验。
Study on Software of Solid Propellant Burning Rate Prediction Based on one-dimensional Steady-state Reaction Gas Flow
基于一维气相稳态反应流的燃速预估软件研究
The atomization mechanism of hypergolic rocket propellant and decomposition combustion at high pressure and turbulence burning of premixed reactant flow field are considered.
数值仿真模型中考虑了自燃推进剂雾化机理、高压分解燃烧和预混反应流湍流燃烧等。
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