2) Solid fuel ramjet-assisted projectile
固冲增程炮弹
1.
Solid fuel ramjet-assisted projectile was numerically analyzed by using the software Fluent as platform to solve the three-dimensional Navier-Stokes equations,and the flow-field construction and the resistance characteristic of the ramjet-assisted projectile were analysed comparatively.
为进一步进行优化设计,提高冲压增程炮弹性能,建立了冲压增程炮弹的三维计算模型,采用Navier-Stokes理论、以Fluent流场计算软件为平台对固冲增程炮弹进行了三维流场数值仿真。
3) ramjet-assisted projectile
冲压增程炮弹
1.
Numerical simulation and analysis for flow field of ramjet-assisted projectile
冲压增程炮弹流场数值仿真与分析
4) ramjet assisted range projectile
冲压增程弹
1.
An inlet has been designed for ramjet assisted range projectile.
以冲压增程弹为应用背景进行了进气道设计。
5) solid fuel ramjet
固体燃料冲压发动机
1.
Analysis on thrust stationarity and flight stability of solid fuel ramjet;
固体燃料冲压发动机推力平稳性及飞行稳定性分析
2.
Influence of vortex on performance of solid fuel ramjet;
涡流对固体燃料冲压发动机性能影响分析
3.
Structure design on torch igniter of solid fuel ramjet;
固体燃料冲压发动机火炬式点火器设计
6) Solid fueled ramjet
固体燃料冲压发动机
1.
Based on theorctical analysis of mean burning rate in solid fueled ramjet (SFRJ),the exponcntialrelationship between burning rate and chamber diameter and pressure is established through numerical simula-tion.
在固体燃料冲压发动机（SFRJ）平均燃速理论分析基础上，通过数值摸拟，得出燃速与燃烧室直径和压强的指数表达式。
2.
Simple reacting flow model of solid fueled ramjets based on Arrenius formula and viscosity hydrodynamics is established and used to simulate an experimental ramjet.
建立了基于阿累尼乌斯公式和粘性流体力学的固体燃料冲压发动机（ＳＦＲＪ）简单反应流模型，并在该模型下对某实验发动机进行了模拟，得出了燃烧剂组分、燃速、温度等发动机参数的变化趋势，给出了一些有用的结论。
补充资料：固体燃料
分子式：
CAS号：
性质：产生热能或动力的固态可燃物质。大都含有碳或碳氢化合物。天然的有木材、泥煤、褐煤、烟煤、无烟煤、油页岩等。经过加工而成的有木炭、焦炭、煤砖、煤球等。此外，还有固体酒精、固体火箭燃料等。燃烧较难控制，效率较低，灰分较多。可直接用作燃料，也可用作制造液体燃料和气体燃料的原料或化工产品的原料。
CAS号：
性质：产生热能或动力的固态可燃物质。大都含有碳或碳氢化合物。天然的有木材、泥煤、褐煤、烟煤、无烟煤、油页岩等。经过加工而成的有木炭、焦炭、煤砖、煤球等。此外，还有固体酒精、固体火箭燃料等。燃烧较难控制，效率较低，灰分较多。可直接用作燃料，也可用作制造液体燃料和气体燃料的原料或化工产品的原料。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条