激波管 的英文怎麼說

中文拼音 [jībōguǎn]
激波管 英文
shock tube
  • 激 : Ⅰ動詞1 （水因受到阻礙或震蕩而向上涌） swash; surge; dash 2 （冷水突然刺激身體使得病） fall ill fr...
  • 波 : Ⅰ名詞1 （波浪） wave 2 [物理學] （振動傳播的過程） wave 3 （意外變化） an unexpected turn of even...
  • 管 : Ⅰ名詞1 （管子） pipe; tube 2 （吹奏的樂器） wind musical instrument 3 （形狀似管的電器件） valve;...
  1. Hypersonic shock tube

    高超聲速激波管
  2. Shock tube ; conical convergent section ; detonation ; finite volume tvd scheme

    激波管收縮截面爆轟有限體積tvd格式
  3. The numerical simulation of axisymmetric two - dimensional shock tube is studied, which has a conical convergent section, and its driving gas is the hot product of hydrogen oxygen detonation. finite volume tvd scheme is adopted and the mesh is local orthogonal. the primitive equations are euler s equations of multi - component flow. the new method of eliminating numerical oscillation at the interface of two materials is extended to two dimensions. the mechanical character of this shock tube is analyzed

    對由前向爆轟產生驅動氣體並具有局部錐形收縮截面的軸對稱激波管利用兩相常比熱完全氣體的歐拉方程組和有限體積tvd格式在局部正交的網格上進行了二維數值模擬。將消除兩種介質界面處數值振蕩的新方法成功地推廣到二維情況。分析了該激波管的力學特性。
  4. In the shock tube, the detonation parameters, such as critical initiation energy, detonation velocity, detonation pressure, detonation limitation and etc., have been measured and the relation is too obtained between detonation parameters and equivalence ratio. chemical kinetics process of hydrocarbon fuel has been analyzed according to the chain reaction mechanism

    在立式激波管中測試了工業燃料c _ 5h _ （ 8 . 68 ）的臨界起爆能、爆速、爆壓、爆轟極限，得到了爆轟參數與當量比之間的關系；從爆轟反應是一個鏈反應機理出發，分析碳氫燃料的反應動力學過程。
  5. In this dissertation, the pulse jet style, the influence on the shock wave, the flow in the tube and the cooling effect was deeply studied theoretically and experimentally. the influence of the pulse jet style on the forming of shock wave and the shock wave intensity was explored. the initial disconnection style in oscillating tube vented and the initial disconnection breakdown was proposed by different pulse jet style

    本文對脈動射流的型式及其對激波、管內流動及冷效應的影響進行了較系統的理論和實驗研究，主要包括:探討了脈動射流的型式對形成管內激波形成及激波強度的影響，給出了不同脈動射流的型式下振蕩管開口端初始間斷的類型，對初始間斷進行了分解，導出了包含進氣、排氣參數及工質物性參數的管內入射激波馬赫數mj的表達式，給出了管內激波形成的三種原因及其所對應的脈動射流型式和具體的工作狀態。
  6. Data of response of three high - pressure transducers are acquired respectively with effect of gas - shock tube and quick - opening valve. dynamic characters of transducers are known fully because of complementarity of data when transducers are calibrated at different frequency bands and pressure ranges. characteristic of excitation signal and its influence for modeling are discussed in this paper

    將三種高壓傳感器在氣體激波管和快速閥門上分別得到激勵響應的數據，根據兩者所能校準的頻率段和壓力范圍不同，利用數據的互補性，可以對傳感器的動態特性有全局的了解。
  7. 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，該風洞可以採用炮風洞和激波管兩種運行方式。
  8. The cellular structures width of po in the shock tube in atmospheric pressure and negative pressure condition has been measured. due to different condition, the figurations of the cellular structure obtained are either regular or irregular respectively. the relation between the cellular width and equivalence ratio is " u " shape

    在常壓和負壓兩種條件下測試了環氧丙烷（ po ）在激波管中的胞格尺寸，分別測得了規則和不規則的胞格結構煙跡，得出了胞格寬度與當量比是「 u 」型曲線關系的結論；並分析了雲霧爆轟的反應機理。
  9. An experimental study of blast waves propagating in liquid sprays is described. it is conducted in a vertical tube with 5. 4m long, 0. 2m inner diameters

    在長5 . 4米，內徑0 . 2米的立式激波管上，進行爆炸波在液霧中的傳播規律的實驗研究。
  10. A numerical investigation is carried out for the phase change in the unsteady expansion of humid gases

    摘要採用數值方法對激波管非定常膨脹過程中，汽液相變與流場的相互作用進行了模擬。
  11. Shock tube wind tunnel

    激波管風洞
  12. Simulation of axisymmetric two - dimensional shock tube driven by hydrogen oxygen detonation

    軸對稱二維氫氧爆轟驅動激波管的模擬
  13. In this thesis, a 2 - d axial symmetric n - s equation was solved by using steger - warming flux splitting, muscl, b - l model and finite volume method to simulate an experiment, which was to observe explosion phenomenon

    本文用steger - warming分裂和b - l湍流模型的有限體積演算法求解二維軸對稱navier - stokes方程，數值模擬了錐形激波管中爆炸波運動和爆炸波正壓和負壓脈沖。
  14. The static pressure distributions of turbine blade surface were measured under five different circumstances and heat flux distributions of turbine blade were measured under two different circumstances. the experiment ' s accuracy, reliability were discussed

    對激波管風洞實驗臺的測試精度、可靠性進行討論表明該種實驗方式對渦輪流場測壓、測熱實驗具有令人滿意的精度。
  15. The flow field and the temperature field in the turbine cascade were studied in view of experiment and computation. using the shock wind tunnel, two kinds of turbine cascade were tested

    本文在激波管風洞中利用兩種葉柵在總共五種工況下進行了葉表靜壓測量實驗，在兩種工況下進行了葉表熱流率測量實驗。
  16. It can show the process of calibrating sensors by using shock tube and show the dynamic performance of sensors

    較完整的實現了用激波管校準傳感器的模擬過程，展示傳感器的動態特性。
  17. Explosives for civil uses - detonators and relays - determination of resistance to cutting damage of leading wires and shock tubes

    民用爆炸物.雷管和傳爆管.引線和激波管耐切割損壞的測定
  18. Shock tube virtual testing system is indispensable part of the virtual system of testing sensor ' s dynamic performance

    激波管虛擬實驗平臺是傳感器動態特性虛擬實驗系統的一個必要組成部分。
  19. Explosives for civil uses - detonators and relays - part 23 : determination of the shock - wave velocity of shock tube ; german version en 13763 - 23 : 2002

    民用爆炸物.雷管和繼電器.第23部分:激波管激波速度的
  20. Explosives for civil uses - detonators and relays - part 24 : determination of the electrical non - conductivity of shock tube ; german version en 13763 - 24 : 2002

    民用爆炸物.雷管和繼電器.第24部分:激波管非導電性的
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