固体燃料冲压发动机,solid fuel ramjet
1)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
英文短句/例句

1.Numerical Simulation of Combustion Characteristic in Combustion Chamber of SFRJ固体燃料冲压发动机燃烧室燃烧特性数值模拟
2.Numerical Simulation of Interior Flow Field in SFRJ固体燃料冲压发动机内流场数值模拟
3.Numerical analysis on two types of afterburning chamber for solid fuel ramjet固体燃料冲压发动机两种补燃室构型数值分析
4.Experiment on swirl combustion characteristics of solid fuel ramjet固体燃料冲压发动机旋流燃烧特性试验
5.Numerical simulation of cold swirl flow field for solid fuel ramjet固体燃料冲压发动机旋流冷流流场数值模拟
6.Combustion Performance Numerical Analysis on Two Styles of Inner Bypass for Solid Fuel Ramjet固体燃料冲压发动机两种内旁路构型燃烧性能数值分析
7.Effect of High Speed Spinning of Solid Fuel Ramjet on Steady Operation Range of Its Inlet固体燃料冲压发动机高速旋转对进气道稳定工作范围的影响
8.The Research on Characteristic Performance of Combustion Flow Field in Secondary Combustion Chamber for Extended Range Solid Rocket Ramjet增程固体火箭冲压发动机补燃室燃烧特性研究
9.liquid-fuelled ramjet engine液体燃料冲压喷气发动机
10.Ignition experimental for liquid hydrocarbon fueled scramiet with simulated flight Mach 4Ma=4液体碳氢燃料超燃冲压发动机点火试验
11.Effects of Jet Rotational Angle on the Second Combustor of Boron-based Propellant Solid Rocket Ramjets含硼固体火箭冲压发动机中燃气旋流角对补燃室的影响
12.Dynamic Properties Research of a Liquid Fuel Ramjet Engine at High Altitude and High Speed高空高速液体燃料亚燃冲压发动机动力特性研究
13.Experimental study on the combustion and flow process in a scramjet with strut injector超燃冲压发动机支板喷射燃料的燃烧过程试验
14.Research on Thermal Protecting of Afterburning Chamber for Integral Solid Rocket-ramjet固体火箭冲压发动机补燃室梯度热防护体系研究
15.Research on the Secondary Combustion Chamber Operation Process of Boron-Based Propellant Ducted Rockets;含硼推进剂固体火箭冲压发动机补燃室工作过程研究
16.Three-Dimensional Numerical Simulation of Afterburner Flow Field of Solid Rocket Ramjet固体火箭冲压发动机补燃室流场三维数值计算研究
17.Experimental investigation on self-sustaining combustion of powdered metal fuel ramjet粉末燃料冲压发动机自维持稳定燃烧试验研究
18.A New Type of Solid Rocket Engine Fuel--Paraffin-based Fuel一种新型固体火箭发动机燃料——石蜡基燃料
相关短句/例句

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。
3)SFRJ固体燃料冲压发动机
1.3-Dimensional Numerical Calculation of Effect of Mass Addition on Whole Internal Flow Fluid of SFRJ;质量加入影响固体燃料冲压发动机统一内流场的三维数值计算
2.SFRJ USED ON MINOR DIAMETER AMMUNITION;固体燃料冲压发动机在小口径弹药上的应用
3.Numerical Simulation of Interior Flow Field in SFRJ固体燃料冲压发动机内流场数值模拟
4)Solid Fuel Ramjet (SFRJ)固体燃料冲压发动机
1.For the excellent characters of simple configuration, high specific impulse and low cost, Solid Fuel Ramjet (SFRJ) has become the preferred power system for the next long-range and ultralong-range projectiles.固体燃料冲压发动机(SFRJ)以其结构简单、比冲高、成本低等优点,目前已成为下一代远程及超远程增程炮弹的首选动力装置。
5)performance of SFRJ固体燃料冲压发动机性能
6)solid-fuel ramjet固体燃料冲压喷气发动机<火>
延伸阅读

冲压式喷气发动机燃料分子式:CAS号:性质:用于冲压式喷气发动机的航空喷气燃料。冲压式喷气发动机是超音速飞行发动机(1200km/h以上),故要求其燃料发热量高、密度大、蒸气压低和热稳定好。适用的品种有石油馏分煤油和高密度烃类燃料(密度多为0.8~0.95g/cm3)。