| 单词 | scramjet |
| 释义 |
复数：scramjets 例句释义: 超音速冲压式喷气发动机[飞机],超燃冲压发动机,超音速燃烧冲压发动机,超音速燃烧冲压引擎 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. As part of this effort, an integrated scramjet model is about to begin testing at up to Mach 5. 6 in a new wind tunnel in Beijing. 作为该项工作的一部分，一个可达5.6马赫的综合冲压模型即将在北京的一个新的风洞内开始测试。 dict.bioon.com 3. A scramjet engine goes as fast as a rocket, but it doesn, t have to carry its own oxygen supply. 超音速燃烧冲压式喷气发动机能使飞行像火箭一样快，但它不必自携氧气。 blog.sina.com.cn 4. America's armed forces see potential in hypersonic aircraft, which fly at Mach 5 or faster using a type of engine known as a scramjet. 美国军方也注意了超音速飞机的潜在价值，若配置超燃冲压引擎，战机巡航速度可以达到5马赫甚至更快。 www.ecocn.org 5. An experimental study was carried out on three-dimensional scramjet inlet flow. 本文主要进行超燃冲压发动机三面压缩进气道的实验研究。 sylx.ustc.edu.cn 6. Earlier this week, the Air Force announced that the X-51 WaveRider, a wingless scramjet, would make its first hypersonic flight. 本周初，美国空军宣布，超音速冲压喷射发动机驱动的X-51“驭波者”将进行其首次超音速飞行。 www.techcn.com.cn 7. In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed. 最后，本文针对两种构型的超音速尾喷管，对其流场进行了计算和分析。 www.fabiao.net 8. Scramjets might someday even power long-range hypersonic passenger airliners, permitting, say, a two-hour flight from New York to Sydney. 甚至，scramjet有朝一日可望用来推进长程的超音速客机，从纽约到雪梨只要两个小时。 192.192.169.81 9. The results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel . 计算研究表明，在相同的来流条件下，供油规律对燃烧室的工作模态有着重大的影响； www.fabiao.net 10. "The facility is to provide high enthalpy [thermal dynamic] model scramjet testing, " he says. “该实验室将提供高焓值[热动力学]模型超燃冲压发动机测试，”他说。更详细。 dict.bioon.com 1. After learning that the scramjet would reach Mach 6, we couldn't help but reflect on the progress aviation has made in just a century. X-51的速度将达到6马赫（6倍音速），让我们惊叹之余，不由得要回顾一下航空科技在短短一个世纪内取得的进展。 www.bing.com 2. Dual-Mode combustion chamber , as the key component of the Scramjet, is the most difficult to design. 双模态燃烧室是双模态超燃冲压发动机中最关键的部件和设计难点。 www.fabiao.net 3. At last, after decades of intermittent development, practical scramjets appear poised to take wing. 在经过几十年断断续续的发展后，具实用性的scramjet可望展翅而飞。 192.192.169.81 4. In just over 100 years, we've gone from the first powered flight to a scramjet capable of Mach 6. Amazing. 过去短短的100年时间里，从人类第一台动力驱动的飞行器，到速度可达6马赫（6倍音速）的超音速冲压喷射发动机。航空科技的发展成绩斐然。 www.techcn.com.cn 5. The thermal environment of the scramjet strut leading edge is rigorous. 在超燃冲压发动机工作过程中，支板前缘的热环境非常恶劣。 www.ceps.com.tw 6. But how does NASA plan to get the scramjet to the supersonic speeds necessary for sustained flight? 不过，太空署要如何使得超燃冲压发动机进入持续飞行需要的超音速呢？ www.bing.com 7. Once a scramjet is moving fast enough, the jet engine would take over and propel it spaceward. 一旦冲压发动机的运动速度足够快，喷射引擎将接手并将之推动进入太空。 www.bing.com 8. a magnetohydrodynamic (MHD)-controlled inlet is adopted in order to improve the scramjet inlet performance in off-design conditions. 为提高超燃冲压发动机进气道在非设计状态下的性能，对磁控进气道进行了研究。 hkxb.buaa.edu.cn 9. Record-breaking "Scramjet" 破纪录的“超音速燃烧冲压喷气发动机” www.bing.com 10. Numerical study of the cold flowfield of a hydrocarbon fueled model scramjet combustor with a streamwise vortices mixer 碳氢燃料流向涡掺混超燃模型燃烧室冷态流场数值研究 www.ilib.com.cn 1. Experimental and numerical investigation of a forward sweep sidewall compression scramjet inlet with forebody compression 带前体压缩的前掠侧压式进气道实验及数值研究 service.ilib.cn 2. Flow Field Calculation for Designing a Kerosene Heater Used for Scramjet 超燃冲压发动机煤油燃烧加热器设计中的流场计算 service.ilib.cn 3. An efficient method for increasing mass flow capture ratio of a three-dimensional sidewall compression scramjet inlet 一种提高后掠侧压式进气道流量系数的有效措施 service.ilib.cn 4. Effects of Fuel Injection Scheme on the Mixing and Combustion Efficiency of a Scramjet Combustor 燃料引射方式对超燃冲压燃烧室混合及燃烧效率的影响 www.ilib.cn 5. Experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor 碳氢燃料超燃冲压发动机点火技术试验 www.ilib.cn 6. Test of a generic sidewall compression scramjet inlet in the high-enthalpy impulse wind tunnel 高超侧压式进气道高焓脉冲风洞实验 www.ilib.cn 7. Integrated flow field calculation of a modularized scramjet 单模块超燃冲压发动机一体化流场数值计算 www.ilib.cn 8. Numerical simulations of flowfields in a scramjet combustor with a strut 支板构型超燃冲压燃烧室流场数值模拟 www.ilib.cn 9. Impulse combustion wind tunnel and its application in rocket and scramjet research 脉冲燃烧风洞及其在火箭和超燃发动机研究中的应用 www.ilib.cn 10. Spillage characteristics of sidewall compression scramjet inlets 高超声速侧压式进气道溢流特性研究 www.ilib.cn 1. Experimental Investigation of Hydrocarbon-fuel Ignition in Scramjet Combustor 超音速燃烧室碳氢燃料点火实验研究 service.ilib.cn 2. A preliminary study of the arc flow field for scramjet research 超燃冲压发动机电弧加热器试验流场调试 www.ilib.cn 3. Preliminary Investigation of Scramjet Engine Performance 超燃冲压发动机性能初步研究 www.ilib.cn 4. The parallel simulation of the chemical nonequilibrium flows in scramjet 超燃发动机化学非平衡场的并行计算 service.ilib.cn 5. Issues associated with long duration high enthalpy scramjet combustor testing 高焓超音速燃烧冲压喷气发动机燃烧室长期试验的结果 lib.buaa.edu.cn 6. Analysis of the hydrogen combustion field in scramjet dual-cavity combustor 超燃冲压发动机双凹腔燃烧室氢气燃烧流场分析 zhidao.baidu.com 7. Numerical Simulation of Flow fields in a Scramjet Combustor with Two Steps 双台阶超燃冲压发动机燃烧室流场数值模拟 service.ilib.cn 8. Influence Factor Analysis of the MHD Controlled Scramjet Inlet Design 超燃冲压发动机磁控进气道设计影响因素分析 www.ilib.cn 9. Analysis of Comparative Numerical Simulation of Free-jet Scramjet Combustor 自由射流超燃冲压发动机燃烧室流场对比计算研究 www.ilib.cn 10. Numerical Simulation of the Flowfield in a Scaled down Scramjet Combustor 超燃冲压发动机缩比燃烧室流场数值模拟 www.ilib.cn 1. Analysis of design calculation methods of scramjet combustion chamber 超燃冲压发动机燃烧室设计计算方法的研究 www.ilib.cn 2. Primary calculating model for integrated scramjet engine design 一体化超燃冲压发动机初步设计计算模型 www.wenloo.com 3. Numerical simulation of single expansion ramp nozzle for scramjet on the designing point 超燃冲压发动机非对称喷管设计点性能 www.ilib.cn 4. Study on numerical simulation of the dual-mode scramjet combustor 双模态冲压发动机燃烧室流场数值模拟研究 ilib.cn 5. Numerical simulation of single expansion ramp nozzle for scramjet on the off-design point 超燃冲压发动机非对称喷管非设计状态性能计算 www.ilib.cn 6. Variable geometry effects on the scramjet ignition and combustion 变几何喉道对超燃冲压发动机点火与燃烧性能的影响 service.ilib.cn 7. Design and optimization method for two dimensional scramjet inlet 超燃冲压发动机二维进气道优化设计方法研究 www.ilib.cn 8. The Design of Combustion Efficiency Sampling-Probe in. Scramjet Engine 超燃冲压发动机燃烧效率取样探针设计 service.ilib.cn 9. Integrated design and optimization method for scramjet 超燃冲压发动机一体化设计与优化方法研究 www.ilib.cn 10. The Multi-level and Multiobjective Optimization Design Method for Two Dimensional Scramjet Inlet 超燃冲压发动机二维进气道多级多目标优化设计方法 ilib.cn 1. Influence of Injection Mode on Flame Stability in Dual-mode Scramjet Combustor 喷注方式对双模态冲压发动机燃烧稳定性的影响 www.ilib.cn 2. The calculational tool of thermal structure design for regeneratively cooled scramjet 超燃冲压发动机再生冷却热结构设计的计算工具 ilib.cn 3. Testing a model scramjet with fuel supplying in hypersonic pulsed wind tunnel 高超声速脉冲风洞中带燃料的超燃冲压发动机模型试验 ilib.cn 4. Trajectories Analyse for Hypersonic Vehicle with Scramjet Based on Perturbation Atmosphere Model 基于扰动大气模型的动力推进高超声速飞行器弹道特性分析 www.ilib.cn 5. Numerical Simulation for the Fuel Jet and Inner Flowfield of Scramjet Combustion Chamber 燃冲压发动机燃烧室燃料喷注及其内流场的数值模拟 ilib.cn 6. Optimal sensor location of scramjet combustor 超燃冲压发动机燃烧室传感器最佳位置选择 www.ilib.cn 7. Optimization design of two dimensional scramjet nozzle based on N-S equations 二维超燃冲压发动机尾喷管优化设计 www.ilib.cn 8. Research on Flow Characteristic of Isolator in Scramjet 超燃冲压发动机隔离段流动特性研究 ilib.cn 9. Experiment study on supersonic inlet in dual-model scramjet 双模态冲压发动机高超进气道的实验研究 www.ilib.cn 10. Numerical study on normal fuel injection in scramjet 超燃发动机垂直燃料喷射的数值研究 service.ilib.cn 1. Review of scramjet engine development 超燃冲压发动机研究综述 www.wenloo.com 2. Application of control technology based on Venturi in kerosene fueled scramjet 文氏管在煤油燃料超燃冲压发动机中的应用 service.ilib.cn 3. Research on Design of Nozzle in Scramjet 超燃冲压发动机尾喷管设计方法研究 www.ilib.cn 4. New development of scramjet engine in French 法国冲压发动机研究进展 www.ilib.cn 5. Investigation of Flow Field of Nozzle for Scramjet 超燃冲压发动机尾喷管流场研究 www.ilib.cn |
| 随便看 |
|
英汉双解词典包含2704715条英汉词条，基本涵盖了全部常用单词的翻译及用法，是英语学习的有利工具。