| 单词 | ramjet |
| 释义 |
复数：ramjets 例句释义: 冲压喷气,冲压发动机,冲压式喷气发动机,冲压喷气发动机 1. One answer could come from a supersonic combustion ramjet, known as a scramjet, which would scoop oxygen from the atmosphere as it ascends. 有一个可能的解决方法，就是超音速燃烧冲压喷射引擎（supersoniccombustionramjet，简称scramjet），它在升空时会努力从大气吸入氧氧。 192.192.169.81 2. The propellant which has higher density special impulse can be applied into ramjet which has no nozzle. 具有较高密度比冲的高能推进剂可用于无喷管推进的冲压发动机中。 paper.pet2008.cn 3. MODEL 79 Meanwhile, McDonnell continued to seek an outlet for the principles and design simplicity developed in the XH-20 ramjet helicopter. 模型79与此同时，麦继续寻求出路的原则和设计开发的简单新华-20喷气直升机。 www.tech-domain.com 4. The investigation lays a fine foundation for realizing stable high efficient combustion based on the thermal throat RBCC ramjet mode. 研究工作为实现基于热力喉道的RBCC亚燃模态稳定高效燃烧提供了良好的基础。 lib.cqvip.com 5. China already has such segmented solid rocket motor and ramjet capabilities today, but scramjets are a much greater challenge. 中国已经拥有这种分离式火箭助推器和冲压发动机技术，但超音速燃烧冲压发动机是一个更大的挑战。 dictsearch.appspot.com 6. On top was an 18-ft diameter, twin-bladed rotor carrying a 10-lb ramjet burner at each of the tips. 上方是一个18英尺长，直径双转子叶片进行了10磅冲压发动机燃烧在每个秘诀。 www.tech-domain.com 7. Ramjet engine is ideal propulsive equipment for new supersonic missile, and supersonic inlets are important components. 冲压发动机是新一代超声速导弹理想的动力装置，超声速空气进气道是它的一个重要部件。 www.fabiao.net 8. A ramjet airplane engine designed for hypersonic flight that burns fuel in the supersonic airstream produced by the plane. 超音速冲压喷气发动机：一种喷气式飞机发动机，设计用于极超音速飞行，燃料在由飞机产生的超音速气流中燃烧。 bbs.putclub.com 9. The influences of mass warp, aerodynamic resistance warp and solid rocket-ramjet engine thrust warp on the flight velocity are analyzed. 研究了靶弹质量偏差、气动阻力偏差和冲压发动机推力偏差对飞行速度的影响。 paper.pet2008.cn 10. The ramjet performance is calculated and compared with fixed and continuous adjustable structure intake and nozzle in this paper. 本研究对具有固定、连续可调进气道和尾喷管的冲压发动机性能进行了计算和比较。 lib.cqvip.com 1. The firing was intended to verify the missile's ability to transition from rocket-boosted to ramjet-powered flight. 发射计划确认导弹有能力从火箭助推转变到冲压-动力飞行。 www.armsky.com 2. Ramjet combustor with cavity as flameholder has simple configuration and excellent flame hold characteristic. 凹腔作为火焰稳定器具有结构简单、火焰稳定能力强的特点。 paper.pet2008.cn 3. Ramjet engines have traditionally used liquid fuel which is mixed with atmospheric air and burned to provide thrust for high-speed flight. 传统的冲压喷气发动机使用液体燃料并与大气中的空气混合燃烧，以提供高速飞行的推力。 www.bing.com 4. To solve this problem, the steady internal flow field of ramjet inlets at different boundary conditions was simulated and analyzed. 针对这一问题，对冲压发动机进气道进行了不同边界条件下的数值模拟，对稳态流场结果进行了分析。 www.ceps.com.tw 5. the simulation model of operation process of solid fuel ramjet was established. 建立了固体燃料冲压发动机工作过程仿真模型。 www.juyy.net 6. The rockets give the planes and missiles enough speed to make the ramjet engine workable. 这种助推火箭为飞机和导弹提供足够的速度，以使冲压式喷气发动机可以开动工作。 www.dictall.com 7. These include a combined solid-motor, ramjet-powered PL-21. 这些包括以混合固体燃料冲压发动机为动力的PL-21。 www.ptfcn.com 8. As a result, the process of organizing combustion is important to realize the best performance of water ramjet engine. 因此，水冲压发动机燃烧组织过程的好坏是其性能优势能否得到充分发挥的关键。 paper.pet2008.cn 9. The SH-5 was originally scheduled to carrying the YJ-1 (C-101) supersonic ramjet-powered anti-ship missile for surface strike role. 5本来预定为水面打击角色携带YJ-1（C-101）超音速冲压发动机反舰导弹。 www.armsky.com 10. The missile, with a single inlet for the ramjet, may have undergone ground tests last year. 这款使用单进气道冲压发动机的导弹，可能已经在去年进行了地面试验。 www.ptfcn.com 1. Ignition Experimental Study of a Variable Geometrical Throat Dual-mode Ramjet 几何可调喉道双模态冲压发动机点火过程试验研究 www.ilib.cn 2. Experimental study of a variable-area propelling nozzle dual-mode ramjet 可调喷口双模态冲压发动机试验研究 www.ilib.cn 3. Characteristic study of an inlet flow-through drag reduction method on solid-ramjet engine 一种固冲组合发动机进气道通气减阻方案的特性研究 www.ilib.cn 4. Study of the influence of environment to the performance of ramjet ignition device 环境对冲压发动机烟火点火器性能影响研究 www.ilib.cn 5. Numerical Simulation on the Inlet Complex Turbulent Flow of Ramjet Assisted Range Projectiles 冲压增程弹丸进气道复杂湍流流场数值仿真 service.ilib.cn 6. Numerical Simulation on Inlet Complex Flow of Ramjet Assisted Range Projectiles with Zonal Method 冲压增程弹丸进气道内外流场分区数值模拟 www.ilib.cn 7. Numerical study of the throttle characteristic about the ramjet inlet and mixing section 冲压发动机进气道和掺混段节流特性数值研究 www.ilib.cn 8. Genetic algorithm applied to integral design optimization of missile propelled by solid rocket ramjet 固体火箭冲压发动机导弹一体化遗传算法优化设计 ilib.cn 9. Effects of the air inlet angle and jet number on mixing flow in the afterburning chamber of solid rocket ramjet 喷口数与进气道角对固冲发动机补燃室气流掺混的影响 service.ilib.cn 10. Application of TTM grids on the research of inlet complex flow of ramjet assisted range projectile 应用TTM网格研究冲压增程弹丸进气道内外流场 www.ilib.cn 1. Experimental study of mixing flow in afterburning chamber of solid rocket ramjet in cold flows 固体火箭冲压发动机补燃室冷态流场实验研究 www.ilib.cn 2. Numerical study of the ramjet engine inner flow before ignition 冲压发动机点火前内流场数值仿真研究 168.160.184.78 3. system capability estimating for a metal water reaction fuel ramjet system 水反应水冲压发动机系统性能估算 www.ichacha.net 4. Viscous pressure forming of super-alloy super-thin wall corrugated parts applied to ramjet engine 冲压发动机超薄壁波纹形件的粘性介质压力成形 www.ilib.cn 5. Numerical simulation of effect of disturbing on starting state of ramjet engine inlet 扰动对超声速进气道起动状态影响的数值模拟 www.ichacha.net 6. Analysis of the Engine Performance for the Ramjet Extended Range Projectile 冲压增程炮弹发动机工作性能分析 www.ilib.cn 7. Contrast study on cold-flow mixing effect and combustion efficiency of afterburning chamber of solid rocket ramjet 固冲发动机补燃室冷流掺混效果与燃烧效率对比研究 www.ilib.cn 8. Numerical investigation for the effect of spinning velocity on high speed spinning ramjet assisted range projectile inlet 转速对高速旋转冲压增程弹用进气道影响数值模拟 www.ilib.cn 9. Numerical Simulation of Three-Dimensional Flows in a Ramjet Combustor 冲压发动机燃烧室三维流场数值模拟 www.ilib.cn 10. Numerical simulation of mixing and combustion flow field in afterburning chamber for solid rocket ramjet 固体火箭冲压发动机补燃室掺混与燃烧流场数值模拟 ilib.cn 1. Numerical simulation on complex flow field in air inlet of high-speed spinning ramjet extended range projectile 高速旋转冲压增程弹用进气道复杂流场数值模拟 www.ilib.cn 2. Numerical simulation for ramjet cruising stage fuel-supplied oscillation 某型弹用冲压发动机巡航段供油振荡的数值仿真 www.ilib.cn 3. Numerical Analysis on Flow Field Characteristic of Ramjet Assisted Range Projectile 冲压发动机增程榴弹绕流流场数值分析 www.ilib.cn 4. Computation of two-phase flow with droplet vaporization in ramjet 冲压发动机伴随蒸发过程的两相流流场计算 www.ilib.cn 5. Theoretical performance analysis of the powdered fuel ramjet 粉末燃料冲压发动机理论性能分析 www.ilib.cn 6. Numerical Simulation of Non-Reactive Flow Field for Rotating Ramjet Ram-Compressed Rotor Disc Cavity 旋转冲压发动机冲压转子盘腔冷态流场数值模拟 www.ilib.cn 7. Numerical simulation on turbulent flow in ramjet chamber with central inlet swirl injection 中心进气旋转射流冲压燃烧室湍流流动数值模拟 www.ilib.cn 8. Experimental and Numerical Research on Inlet of Ramjet Assisted Range Projectiles 冲压增程弹用进气道试验与数值研究 www.ilib.cn 9. Digital electronic control system of a liquid fuel ramjet engine 液体冲压发动机数字电子控制系统换 www.ilib.cn 10. Interior Ballistics Calculation for Nozzleless Booster with Solid Propellant Rocket Ramjet Engine 固体火箭冲压发动机无喷管助推器性能分析 ilib.cn 1. Computation of ablation of thermal-protection layer in solid rocket ramjet combustor 固体火箭冲压发动机燃烧室热防护层烧蚀计算 www.ilib.cn 2. Progress of Research on Trapped Vortex Combustion Technology in Rotated Ramjet 旋转冲压发动机驻涡燃烧技术研究现状分析 ilib.cn 3. Influence of air mass flow rate ratio on combustion efficiency of solid rocket ramjet with two air inlets 二次进气流量比对固冲发动机燃烧效率的影响 service.ilib.cn 4. Artificial Neural Network Identification of Burning Rate in Solid Fuel Ramjet 固体燃料冲压发动机燃速的人工神经网络辨识 ilib.cn 5. Analysis on inlet performance of ramjet assisted range projectiles 冲压增程弹丸进气道特性分析 service.ilib.cn 6. Thermodynamic calculation for water ramjet 水冲压发动机热力计算 www.ilib.cn 7. all of the work made foundation of developing solid rocket - ramjet engine 为固体火箭冲压发动机试验研究打下基础。 www.ichacha.net 8. Modelling and Energy Consumption Analysis of Turbopump in Ramjet 冲压发动机涡轮泵建模及能耗分析 www.ilib.cn 9. Configuration of Rotating Ramjet Ram-Compressed Rotor 旋转冲压发动机冲压转子的结构特点 www.ilib.cn 10. Numerical simulation and utilization of inner flow field for solid ramjet 固冲发动机三维内流场数值计算与应用 www.ilib.cn 1. Influence of Inlet Conditions on Thrust and Specific Impulse of Solid Fuel Ramjet 入口条件对固体燃料冲压发动机推力和比冲的影响分析 scholar.ilib.cn 2. Flow rates calculation of combustion heater for ramjet test facility 冲压发动机试车台空气燃烧加热器流量参数计算 www.ilib.cn 3. Applications of gas generator in ramjet direct-connect test facility 加热器在冲压发动机试验技术中的应用研究 www.ilib.cn 4. Ground test equipment and measurement-control system of solid rocket- ramjet engines 固体火箭冲压发动机地面试验装置及测控系统 service.ilib.cn 5. Flight Performance Analysis of the Solid Fuel Ramjet 固体燃料冲压发动机飞行性能分析 ilib.cn 6. Dynamical stress analysis of ram-compressed rotor of rotated ramjet 旋转冲压发动机冲压转子动应力分析 ilib.cn 7. Large eddy simulation on scalar transport in ramjet dump combustor 冲压发动机突扩燃烧室内标量输运的大涡模拟 www.ichacha.net 8. Research on the Integrated Control and System Design of Ramjet Missile 冲压发动机导弹协调控制与总体设计一体化研究 www.ilib.cn 9. Performance Analysis of the Liquid Fuel Ramjet 液体冲压发动机特性分析 www.ichacha.net 10. Research of new conceptive rotated ramjet 新概念旋转冲压发动机的研究与分析 www.ilib.cn 1. Analysis of the unstart boundary for ramjet inlets 冲压发动机进气道不起动边界分析 www.ilib.cn 2. Simple Reacting Flow Simulation of Solid Fueled Ramjet 固体燃料冲压发动机简单反应流模拟 www.ilib.cn 3. Numerical simulation of ramjet inlet flow fields 冲压发动机进气道流场数值模拟 scholar.ilib.cn 4. Combustion Effect on the Reattachment Point in Solid Fuel Ramjet 燃烧对固体燃料冲压发动机附着点的影响 www.ilib.cn 5. Flowfield computation in rocket ramjet with complex boundary 具有复杂边界的火箭冲压发动机流场数值计算 www.ilib.cn 6. Gas Flow Control Technique of Rocket Ramjet 固体火箭冲压发动机燃气流量调节技术与实验研究 www.ilib.cn 7. Research progress of solid fuel ramjet 固体燃料冲压发动机研究进展 www.ichacha.net 8. Inlet Design of Missile with Ramjet Engine 冲压发动机导弹进气道设计的几个问题 www.ilib.cn 9. Numerical analysis on non-premixed combustion of water ramjet 水冲压发动机掺混燃烧数值分析 www.ilib.cn |
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