Chinese translation for "wave intensity"
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- 波的强度
波浪强度
Related Translations:
- Example Sentences:
| 1. | The characteristic of the forming of shock wave in the tube and the influence of the shock wave intensity on cooling effect was also analyzed in working time . the reason why the cooling efficiency was lower in low rotate speed and has no change in high rotate speed was revealed
分析了振荡管实际工作时管内激波形成特点及激波强度对冷效应的影响,指出了实际压力波制冷机在低转速下运行时制冷效率很低而在高转速下制冷效率变化不大的内在原因。 | | 2. | 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
本文对脉动射流的型式及其对激波、管内流动及冷效应的影响进行了较系统的理论和实验研究,主要包括:探讨了脉动射流的型式对形成管内激波形成及激波强度的影响,给出了不同脉动射流的型式下振荡管开口端初始间断的类型,对初始间断进行了分解,导出了包含进气、排气参数及工质物性参数的管内入射激波马赫数mj的表达式,给出了管内激波形成的三种原因及其所对应的脉动射流型式和具体的工作状态。 | | 3. | With account for the effect of temperature and shock - boundary layer interaction , the forebody / inlet with plane lip and wedge lip are designed by using the design methods of constant shock wave intensity and constant shock wave angle . in the design , the incidence angle of the first ramp , height of isolator , length of forebody and total turning angle of the designed forebody / inlet models are given
另外，根据优选结果，给定前体长度、前体预压缩楔角、总压缩转角及隔离段高度，分别用等激波强度和等激波角度的方法设计了唇口平直和唇口带楔角的前体进气道。 | | 4. | The calculation results indicate that the starting performance of forebody / inlet with wedge - shaped lip is better than that with plane lip at low flight mach number . at high flight mach number , the performance of the forebody / inlets designed by the two methods is approximate . at low flight mach number , the starting performance of forebody / inlet designed by the method of constant shock wave intensity is better
结果表明：唇口带楔角的进气道在低飞行马赫数下的起动性能优于唇口平直的进气道；采用等激波强度和等激波角度方法设计的进气道在高飞行马赫数下的性能相近，在低飞行马赫数下，采用等激波强度方法设计的进气道起动性能较优。 |
- Similar Words：
- "wave induced oscillation" Chinese translation, "wave induced shearing force curve" Chinese translation, "wave induced stress" Chinese translation, "wave instability" Chinese translation, "wave inte ity" Chinese translation, "wave interaction" Chinese translation, "wave interference" Chinese translation, "wave interference error" Chinese translation, "wave interference ripple mark" Chinese translation, "wave knives and sticks" Chinese translation
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