H - U英文單字1000 - hypersonic 中文

hypersonic adj.高超音速的〔指超音速五倍以上者〕。

adj. 高超音速的〔指超音速五倍以上者〕。 “aerodynamics; hypersonic“ 中文翻譯：極音速空氣動力學“aircraft; hypersonic“ 中文翻譯：極音速飛機“all-hypersonic“ 中文翻譯：純高超音速的“hypersonic ablation“ 中文翻譯：高超音速燒蝕“hypersonic acceleration“ 中文翻譯：高超音速加速度“hypersonic aerodynamics“ 中文翻譯：超聲空氣動力學; 高超聲速空氣動力學; 高超音速空氣動力學; 極音速空氣動力學; 特超聲速空氣動力學“hypersonic aeroplane“ 中文翻譯：高超音速飛機“hypersonic aircraft“ 中文翻譯：高超音速飛機“hypersonic airplane“ 中文翻譯：特超音速飛機“hypersonic analyzer“ 中文翻譯：超聲波探傷器“hypersonic body“ 中文翻譯：高超音速機身“hypersonic bomber“ 中文翻譯：高超音速轟炸機“hypersonic characteristics“ 中文翻譯：高超音速特性“hypersonic continuum“ 中文翻譯：高超音速流動的連續介質“hypersonic decelerator“ 中文翻譯：高超音速減速裝置“hypersonic density“ 中文翻譯：高超音速時的密度“hypersonic eed“ 中文翻譯：高超聲速“hypersonic engine“ 中文翻譯：高超音速發動機“hypersonic era“ 中文翻譯：高超音速時代“hypersonic facility“ 中文翻譯：高超音速試驗裝置“hypersonic flight“ 中文翻譯：高超音速飛行; 極音速飛行“hypersonic flow“ 中文翻譯：超空間; 高超聲速流[動]又稱“高超音速流[動]”。; 高超音速流動; 極音速流; 特超音速憐“hypersonic flutter“ 中文翻譯：高超音速顫振“hypersonic wave“ 中文翻譯：特超聲波“hypersomnolence“ 中文翻譯：過度嗜睡“hypersomnia-sleep apnea“ 中文翻譯：睡眠過度-睡眠呼吸暫停

hypersonic transport
On a recent project , for example , i ran my persistence unit tests inside of eclipse using hsql and local datasources against a hypersonic sql database using hibernate transaction manager 比如在最近的項目中，我在eclipse中，使用hsql和本地數據庫對使用hibernate事務管理器的hypersonic sql數據庫進行持久性單元測試。
The results show that to design a supersonic / hypersonic nozzle of wind tunnel must consider the effect of variable specific heat , which gives reference to nozzle and wind tunnel design 考慮這一因素后，噴管出口馬赫數接近設計馬赫數，其設計精度有較大提高。本方法可為超音速高超聲速噴管設計和反設計提供參考。
This paper presents the development and preliminary application works of an automatic strain gauge balance static calibration system in ecs for 1m hypersonic wind tunnel of cardc 本文論述了cardc超高速空氣動力研究所1m高超聲速風洞配套的新型全自動六分量應變天平地軸系( ecs )校準系統的研制和初步應用研究工作。
And over the next several decades , the scramjet work could eventually provide china with a tactical hypersonic global - strike capability beyond the country ' s strategic ballistic missile force “中國是具備在軍事上和美國競爭的最有潛力的國家，假以時日，中國的區域破壞性軍事技術能夠抵消美國的傳統軍事優勢。 ”
In recent years , the most of new fighters and strategic missiles require fly with supersonic or hypersonic speed , and this make a lot of researchers think much of this kinds of phenomena 近年來，新一代的戰斗機及新型的戰略導彈對超音速、高超音速飛行的要求，引起了國內外許多研究人員對這一類流動的重視。
Rocket - based combined cycle ( rbcc ) will be promising propulsion system to achieve hypersonic flight , and has extensively application foreground in both military and civil usage 火箭基組合循環( rbcc )推進系統是實現高超聲速飛行的最有潛力的動力方案，具有廣泛的軍事和民用航天應用前景，因而備受矚目。
Using axisymmetric full navier - stokes equations , the thermo - chemical nonequilibrium flow in hypersonic nozzle was simulated and the scale effects due to nonequilibrium were analysed numerically 摘要采用軸對稱熱化學非平衡全n - s方程，數值分析了高超聲速噴管流場中非平衡引起的尺度效應。
Employing euler based steady solution and piston theory , a new method ( we call it local piston theory in this paper ) to solve supersonic or hypersonic unsteady loads has been developed 發展了一種運用定常cfd方法和活塞理論求解超音速、高超音速非定常氣動力的新方法?當地流活塞理論。
Using above methods to solve unsteady pressure distribution , coupling structure equations , the supersonic or hypersonic aeroelasticity is simulated in time - domain 運用上述的非定常氣動力求解方法，耦合結構動力學方程，實現超音速、高超音速氣動彈性的模擬。
Using the 3d program , hyten ( hypersonic , throat - ejecting ) nozzle , which is one of the three latest nozzles first designed in this paper , has been simulated 利用建立的三維模擬程序，對本文設計的新噴管? ?喉部引射注入的高超音速噴管( hyten )和光腔進行了數值模擬。
The software fluent was employed and the two - dimensional flow field and performance parameters of four hypersonic / inlet models at design and off - design condition are obtained 采用fluent軟件對所設計的進氣道設計點和非設計點二維流場和性能進行了數值模擬。
The airframe and engine highly integration nature of hypersonic vehicle results in the asymmetry and cowl adjustable characters of the scramjet nozzle 由于高超聲速飛行器機體與發動機高度一體化的構型,使超燃沖壓發動機尾噴管具有非對稱,面罩可調等特點。
In order to solve the complicated supersonic / hypersonic turbulence viscous flow field , a program for steady flow is built by using implicit lu - sgs method 建立了應用隱式lu - sgs方法的三維定常流動模擬程序,可用于求解超聲速/高超聲速粘性復雜流場。
With the progress of the research and application of modem aerospace technology , the development of hypersonic air vehicles has been pushed to a new climax 伴隨著航空宇航技術的研究及應用的不斷發展，高超聲速飛行器的研制逐漸步入高潮。
Control system design for hypersonic vehicles will be complicated by coupling effects between aerodynamics , propulsion , and structure 高超聲速飛行器的飛行控制系統由于空氣動力學、推進系統以及結構之間的相互耦合影響而變得非常的復雜。
A time magazine display at the convention will feature speeches of past republican presidents in tightly controlled beams of hypersonic sound ( hss ) 時代雜志展示了大會將用這種超音速聲音（ hss ）的緊密的控制的柱來放映前共和黨總統的演講。
With the progress of the research and application of modern aerospace technology , the development of hypersonic vehicles has been pushed to a new climax 伴隨著航空宇航技術的研究及應用的不斷發展,高超聲速飛行器的研制逐漸步入高潮。
A hypersonic pulse tunnel is designed in this paper , which has multiple running modes based on gun tunnel and shock tube theory 本文設計了一座具有多種運行方式的高超聲速大型脈沖風洞,該風洞可以采用炮風洞和激波管兩種運行方式。
During the intercept flying of endo - atmopheric hypersonic vheicles , an infra - red ( ir ) sensor may be used to detect , acquire , and track the target 首先介紹高速飛行的紅外導引頭窗口的溫度分布和窗口周圍的背景輻射計算模型框架。

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hypersonic

hypersonic adj.高超音速的〔指超音速五倍以上者〕。

hypersonic transport

Using above methods to solve unsteady pressure distribution , coupling structure equations , the supersonic or hypersonic aeroelasticity is simulated in time - domain 運用上述的非定常氣動力求解方法，耦合結構動力學方程，實現超音速、高超音速氣動彈性的模擬。

The software fluent was employed and the two - dimensional flow field and performance parameters of four hypersonic / inlet models at design and off - design condition are obtained 采用fluent軟件對所設計的進氣道設計點和非設計點二維流場和性能進行了數值模擬。

The airframe and engine highly integration nature of hypersonic vehicle results in the asymmetry and cowl adjustable characters of the scramjet nozzle 由于高超聲速飛行器機體與發動機高度一體化的構型,使超燃沖壓發動機尾噴管具有非對稱,面罩可調等特點。

In order to solve the complicated supersonic / hypersonic turbulence viscous flow field , a program for steady flow is built by using implicit lu - sgs method 建立了應用隱式lu - sgs方法的三維定常流動模擬程序,可用于求解超聲速/高超聲速粘性復雜流場。

With the progress of the research and application of modem aerospace technology , the development of hypersonic air vehicles has been pushed to a new climax 伴隨著航空宇航技術的研究及應用的不斷發展，高超聲速飛行器的研制逐漸步入高潮。

Control system design for hypersonic vehicles will be complicated by coupling effects between aerodynamics , propulsion , and structure 高超聲速飛行器的飛行控制系統由于空氣動力學、推進系統以及結構之間的相互耦合影響而變得非常的復雜。

A time magazine display at the convention will feature speeches of past republican presidents in tightly controlled beams of hypersonic sound ( hss ) 時代雜志展示了大會將用這種超音速聲音（ hss ）的緊密的控制的柱來放映前共和黨總統的演講。

With the progress of the research and application of modern aerospace technology , the development of hypersonic vehicles has been pushed to a new climax 伴隨著航空宇航技術的研究及應用的不斷發展,高超聲速飛行器的研制逐漸步入高潮。

A hypersonic pulse tunnel is designed in this paper , which has multiple running modes based on gun tunnel and shock tube theory 本文設計了一座具有多種運行方式的高超聲速大型脈沖風洞,該風洞可以采用炮風洞和激波管兩種運行方式。

During the intercept flying of endo - atmopheric hypersonic vheicles , an infra - red ( ir ) sensor may be used to detect , acquire , and track the target 首先介紹高速飛行的紅外導引頭窗口的溫度分布和窗口周圍的背景輻射計算模型框架。