scramjet
美 ['skræm?d?et] 
英 ['skræmd?et]
- n.超音速?zèng)_壓式噴氣發(fā)動(dòng)機(jī)[飛機(jī)]
- 網(wǎng)絡(luò)超燃沖壓發(fā)動(dòng)機(jī)；超音速燃燒沖壓發(fā)動(dòng)機(jī)；超音速燃燒沖壓引擎
詞形變化
復(fù)數(shù)：scramjets
英漢解釋
n. | 1. 超音速?zèng)_壓式噴氣發(fā)動(dòng)機(jī)[飛機(jī)] |
英英解釋
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.
有一個(gè)可能的解決方法，就是超音速燃燒沖壓噴射引擎（supersoniccombustionramjet，簡(jiǎn)稱(chēng)scramjet），它在升空時(shí)會(huì)努力從大氣吸入氧氧。
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.
作為該項(xiàng)工作的一部分，一個(gè)可達(dá)5.6馬赫的綜合沖壓模型即將在北京的一個(gè)新的風(fēng)洞內(nèi)開(kāi)始測(cè)試。
A scramjet engine goes as fast as a rocket, but it doesn, t have to carry its own oxygen supply.
超音速燃燒沖壓式噴氣發(fā)動(dòng)機(jī)能使飛行像火箭一樣快，但它不必自攜氧氣。
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.
美國(guó)軍方也注意了超音速飛機(jī)的潛在價(jià)值，若配置超燃沖壓引擎，戰(zhàn)機(jī)巡航速度可以達(dá)到5馬赫甚至更快。
An experimental study was carried out on three-dimensional scramjet inlet flow.
本文主要進(jìn)行超燃沖壓發(fā)動(dòng)機(jī)三面壓縮進(jìn)氣道的實(shí)驗(yàn)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，美國(guó)空軍宣布，超音速沖壓噴射發(fā)動(dòng)機(jī)驅(qū)動(dòng)的X-51“馭波者”將進(jìn)行其首次超音速飛行。
In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.
最后，本文針對(duì)兩種構(gòu)型的超音速尾噴管，對(duì)其流場(chǎng)進(jìn)行了計(jì)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有朝一日可望用來(lái)推進(jìn)長(zhǎng)程的超音速客機(jī)，從紐約到雪梨只要兩個(gè)小時(shí)。
The results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel .
計(jì)算研究表明，在相同的來(lái)流條件下，供油規(guī)律對(duì)燃燒室的工作模態(tài)有著重大的影響；
"The facility is to provide high enthalpy [thermal dynamic] model scramjet testing, " he says.
“該實(shí)驗(yàn)室將提供高焓值[熱動(dòng)力學(xué)]模型超燃沖壓發(fā)動(dòng)機(jī)測(cè)試，”他說(shuō)。更詳細(xì)。
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的速度將達(dá)到6馬赫（6倍音速），讓我們驚嘆之余，不由得要回顧一下航空科技在短短一個(gè)世紀(jì)內(nèi)取得的進(jìn)展。
Dual-Mode combustion chamber , as the key component of the Scramjet, is the most difficult to design.
雙模態(tài)燃燒室是雙模態(tài)超燃沖壓發(fā)動(dòng)機(jī)中最關(guān)鍵的部件和設(shè)計(jì)難點(diǎn)。
At last, after decades of intermittent development, practical scramjets appear poised to take wing.
在經(jīng)過(guò)幾十年斷斷續(xù)續(xù)的發(fā)展后，具實(shí)用性的scramjet可望展翅而飛。
In just over 100 years, we've gone from the first powered flight to a scramjet capable of Mach 6. Amazing.
過(guò)去短短的100年時(shí)間里，從人類(lèi)第一臺(tái)動(dòng)力驅(qū)動(dòng)的飛行器，到速度可達(dá)6馬赫（6倍音速）的超音速沖壓噴射發(fā)動(dòng)機(jī)。航空科技的發(fā)展成績(jī)斐然。
The thermal environment of the scramjet strut leading edge is rigorous.
在超燃沖壓發(fā)動(dòng)機(jī)工作過(guò)程中，支板前緣的熱環(huán)境非常惡劣。
But how does NASA plan to get the scramjet to the supersonic speeds necessary for sustained flight?
不過(guò)，太空署要如何使得超燃沖壓發(fā)動(dòng)機(jī)進(jìn)入持續(xù)飛行需要的超音速呢？
Once a scramjet is moving fast enough, the jet engine would take over and propel it spaceward.
一旦沖壓發(fā)動(dòng)機(jī)的運(yùn)動(dòng)速度足夠快，噴射引擎將接手并將之推動(dòng)進(jìn)入太空。
a magnetohydrodynamic (MHD)-controlled inlet is adopted in order to improve the scramjet inlet performance in off-design conditions.
為提高超燃沖壓發(fā)動(dòng)機(jī)進(jìn)氣道在非設(shè)計(jì)狀態(tài)下的性能，對(duì)磁控進(jìn)氣道進(jìn)行了研究。
Record-breaking "Scramjet"
破紀(jì)錄的“超音速燃燒沖壓噴氣發(fā)動(dòng)機(jī)”
Numerical study of the cold flowfield of a hydrocarbon fueled model scramjet combustor with a streamwise vortices mixer
碳?xì)?/c>燃料流向渦摻混超燃模型燃燒室冷態(tài)流場(chǎng)數(shù)值研究
Experimental and numerical investigation of a forward sweep sidewall compression scramjet inlet with forebody compression
帶前體壓縮的前掠側(cè)壓式進(jìn)氣道實(shí)驗(yàn)及數(shù)值研究
Flow Field Calculation for Designing a Kerosene Heater Used for Scramjet
超燃沖壓發(fā)動(dòng)機(jī)煤油燃燒加熱器設(shè)計(jì)中的流場(chǎng)計(jì)算
An efficient method for increasing mass flow capture ratio of a three-dimensional sidewall compression scramjet inlet
一種提高后掠側(cè)壓式進(jìn)氣道流量系數(shù)的有效措施
Effects of Fuel Injection Scheme on the Mixing and Combustion Efficiency of a Scramjet Combustor
燃料引射方式對(duì)超燃沖壓燃燒室混合及燃燒效率的影響
Experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor
碳?xì)?/c>燃料超燃沖壓發(fā)動(dòng)機(jī)點(diǎn)火技術(shù)試驗(yàn)
Test of a generic sidewall compression scramjet inlet in the high-enthalpy impulse wind tunnel
高超側(cè)壓式進(jìn)氣道高焓脈沖風(fēng)洞實(shí)驗(yàn)
Integrated flow field calculation of a modularized scramjet
單模塊超燃沖壓發(fā)動(dòng)機(jī)一體化流場(chǎng)數(shù)值計(jì)算
Numerical simulations of flowfields in a scramjet combustor with a strut
支板構(gòu)型超燃沖壓燃燒室流場(chǎng)數(shù)值模擬
Impulse combustion wind tunnel and its application in rocket and scramjet research
脈沖燃燒風(fēng)洞及其在火箭和超燃發(fā)動(dòng)機(jī)研究中的應(yīng)用
Spillage characteristics of sidewall compression scramjet inlets
高超聲速側(cè)壓式進(jìn)氣道溢流特性研究
Experimental Investigation of Hydrocarbon-fuel Ignition in Scramjet Combustor
超音速燃燒室碳氫燃料點(diǎn)火實(shí)驗(yàn)研究
A preliminary study of the arc flow field for scramjet research
超燃沖壓發(fā)動(dòng)機(jī)電弧加熱器試驗(yàn)流場(chǎng)調(diào)試
Preliminary Investigation of Scramjet Engine Performance
超燃沖壓發(fā)動(dòng)機(jī)性能初步研究
The parallel simulation of the chemical nonequilibrium flows in scramjet
超燃發(fā)動(dòng)機(jī)化學(xué)非平衡場(chǎng)的并行計(jì)算
Issues associated with long duration high enthalpy scramjet combustor testing
高焓超音速燃燒沖壓噴氣發(fā)動(dòng)機(jī)燃燒室長(zhǎng)期試驗(yàn)的結(jié)果
Analysis of the hydrogen combustion field in scramjet dual-cavity combustor
超燃沖壓發(fā)動(dòng)機(jī)雙凹腔燃燒室氫氣燃燒流場(chǎng)分析
Numerical Simulation of Flow fields in a Scramjet Combustor with Two Steps
雙臺(tái)階超燃沖壓發(fā)動(dòng)機(jī)燃燒室流場(chǎng)數(shù)值模擬
Influence Factor Analysis of the MHD Controlled Scramjet Inlet Design
超燃沖壓發(fā)動(dòng)機(jī)磁控進(jìn)氣道設(shè)計(jì)影響因素分析
Analysis of Comparative Numerical Simulation of Free-jet Scramjet Combustor
自由射流超燃沖壓發(fā)動(dòng)機(jī)燃燒室流場(chǎng)對(duì)比計(jì)算研究
Numerical Simulation of the Flowfield in a Scaled down Scramjet Combustor
超燃沖壓發(fā)動(dòng)機(jī)縮比燃燒室流場(chǎng)數(shù)值模擬
