scramjet
美 ['skræmˌdʒet] 
英 ['skræmdʒet]
- n.超音速冲压式喷气发动机[飞机]
- 网络超燃冲压发动机；超音速燃烧冲压发动机；超音速燃烧冲压引擎
词形变化
复数：scramjets
英汉解释
英英解释
例句
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。
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。
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。
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。
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。
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。
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。
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。
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；
"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。
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。
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。
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。
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。
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。
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？
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。
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。
Record-breaking "Scramjet"
破纪录的“超音速燃烧冲压喷气发动机”
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
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
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
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
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
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
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
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
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
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
Spillage characteristics of sidewall compression scramjet inlets
高超声速侧压式进气道溢流特性研究
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
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
Preliminary Investigation of Scramjet Engine Performance
超燃冲压发动机性能初步研究
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
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
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
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
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
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
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
