高超音速 的英文怎麼說

中文拼音 [gāochāoyīnsù]
高超音速 英文
[物理學] hypersonic speed高超音速導彈 hypersonic missile; 高超音速飛機 hypersonic aircraft; 高超音速火箭 hypersonic rocket
  • 高 : Ⅰ形容詞1 （從下向上距離大; 離地面遠） tall; high 2 （在一般標準或平均程度之上; 等級在上的） above...
  • 超 : Ⅰ動詞1 （越過; 高出） exceed; surpass; overtake 2 （在某個范圍以外; 不受限制） transcend; go beyo...
  • 音 : 名詞1. （聲音） sound 2. （消息） news; tidings 3. [物理學] （音質） tone 4. （姓氏） a surname
  • 速 : Ⅰ形容詞（迅速; 快） fast; rapid; quick; speedy Ⅱ名詞1 （速度） speed; velocity 2 （姓氏） a surna...
  • 高超 : excellent; exquisite; superb
  • 音速 : [物理學] velocity of sound; speed of sound; sound velocity
  1. Nick collison led seattle with 24 points and 18 rebounds and rookie kevin durant finished with 19 points, but missed 20 shots

    尼克?克里森得到超音速隊最高的24分和18個籃板，新秀杜蘭特也拿到19分，但是卻投丟了20個投籃。
  2. Departures form the ideal practice followed by the wright have been particularly noticeable in the development of supersonic and hypersonic vehicles.

    特別值得注意的是在發展超音速和高超音速飛行器的過程中，偏離了萊特理想的工作方式。
  3. A numerical method for hypersonic aerothermoelasticity

    一種高超音速熱氣動彈性數值研究方法
  4. The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range, lift / drag ratio, and subsonic flight lift / drag ratio, the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc

    摘要介紹了在滿足高超音速再入橫向機動航程，高超音速再入飛行時的升阻比，亞音速進場飛行時的升阻比，縱向靜穩定性裕度和水平著陸速度等飛行性能設計要求下，用罰函數法尋求使航天飛機機翼質量為最小的外形優化方法並給出了算例。
  5. Despite bryant ' s absence, the lakers ( 39 - 17 ) beat the sonics 111 - 91 for their season - high eighth straight victory

    雖然後來沒有科比，但湖人仍以111比91擊敗超音速，取得賽季新高8連勝。
  6. Cross - section design of a controllable hypersonic inlet. the research is being done at the nanjing university of aeronautics and astronautics

    南京航空航天大學正在進行一個可控高超音速進氣道斷面設計研究。
  7. Using local piston theory based on cfd to solve hypersonic unsteady aerodynamic loads, the hypersonic aerothermoelasticity is simulated in time domain

    在時間域內實現了高超音速熱氣動彈性的模擬。
  8. Ramjet has been widely used in all kinds of supersonic and high - supersonic aircraft. it has caught more and more attention recently because there is no need for rotating impeller machine

    而沖壓發動機不需轉動的葉輪機械，結構簡單，高速性能優良，被廣泛用於各類超音速和高超音速飛行器，愈來愈受到人們的關注。
  9. The return of a reusable spacevehicle into earth ' s atmosphere with high - supersonic is gas - heated intensely, which requiring the high performance of thermal protection provided by the hot - structure composite materials

    可重復使用空天飛行器以高超音速再入大氣層時受到強烈的氣動加熱，對結構的防熱性能提出了很高的要求。
  10. The computed flutter speeds are within 10 % of experimentally determined ones

    並在時間域內分析了高超音速氣動彈性的非線性。
  11. With high temperature and high pressure in nozzle of wind tunnel, the effect of variable specific heat on nozzle design must be considered

    本文針對超音速、高超音速噴管內馬赫數、溫度變化劇烈的特點，研究了比熱容變化對設計噴管型面產生的影響。
  12. 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。
  13. 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。
  14. Analyzing existing engineering methods, we combine them in such a way to make computing aerodynamic characteristics possible for arbitrarily shaped body

    驗證、分析了各種超音速、高超音速氣動力工程計算方法，將各種工程方法統一起來，用於求解任意外形的飛行器氣動力。
  15. 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。
  16. 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。
  17. Several non - linear phenomena are also analyzed. by using uncoupled thermal - structure analyzing method, with the consideration the additional stiffness caused by thermal stress, the finite element model for thermal - vibration analysis is obtained and two typical hypersonic wing structures are computed

    運用非耦合熱-結構分析方法，考慮熱應力引起的附加剛度，得到熱環境下的結構分析的有限元模型，並計算了兩種典型結構的高超音速翼面熱結構。
  18. Recently, with the higher and higher requirement of the survival ability of the advanced tactical fighter, supersonic cruise has been required as one of the important performance

    近年來，隨著對戰斗機作戰性能和生存能力要求的不斷提高，超音速巡航已作為戰斗機的一項基本指標。
  19. Using the engineering methods of supersonic and hypersonic flow or local piston theory developed in this paper to compute unsteady aerodynamic loads, and coupling structural equations, the supersonic or hypersonic aeroelasticity with a typical servo system under thermal environment is simulated in time - domain

    運用超音速、高超音速氣動力工程計算方法和本文發展的當地流活塞理論計算非定常氣動力，耦合結構運動方程，實現了熱環境中帶有伺服機構的氣動彈性的時域模擬。
  20. A numerical simulation software is developed that can be used to simulate standing oblique detonation waves in hypervelocity flight conditions. reasonable parameters and advanced method are provided for the application of standing detonation propulsion technology. the main points are as follows : the mathematical model is developed that can be used to analyze the properties of planar standing oblique detonation waves

    通過對駐定斜爆轟波形念的理論分析和數值模擬，對高超音速條件下斜爆轟波的穩定性現象進行了系統研究，探討了產生駐定斜爆轟波的臨界條件，開發了平面和錐形駐定斜爆轟波流場數值模擬軟體，為駐定爆轟推進技術的應用提供合理的系統參數和先進手段。
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