冲击射流的英文

• impact jet flow

• "冲击"英文翻译    lash; pound
• "射流"英文翻译    jet-flow; vein; jet; filamen ...
• "直接冲击射流" 英文翻译 :    direct collision streams
• "冲击射流式喷头" 英文翻译 :    impinging hole injector
• "自冲击射流喷嘴" 英文翻译 :    self impinging injector; self-impinging injector
• "互击射流" 英文翻译 :    impinging jets
• "撞击射流喷咀" 英文翻译 :    impinging-jets burner
• "击射" 英文翻译 :    slap shot
• "射流冲击力" 英文翻译 :    jet impact force
• "直接冲击式射流调制器" 英文翻译 :    direct impact modulator
• "最大射流冲击力工作方式" 英文翻译 :    maximum jet impact force regime; regime of the maximum jet impact force; regime of the maximum jet velocity
• "射流" 英文翻译 :    jet-flow; vein; [物理学] jet; filament band; shooting flow; fluidic; jet current; jet stream; efflux◇射流泵 jet injector; 射流传感器 fluidic sensor; 射流电路 fluidics circuit; 射流管 jet pipe; 射流技术 fluidics; fluidonics; fluerics; 射流喷口 efflux nozzle; 射流速度 efflux velocity; 射流系数 efflux coefficient; 射流装置 fluidic device; fluidizing system
• "大力击射" 英文翻译 :    batting shoot
• "狙击射击" 英文翻译 :    sniper shot
• "冲击" 英文翻译 :    1.(水流等撞击) lash; pound 激流对海岸的冲击 the impact of the swift current against the shore; 海浪冲击着礁石, 飞起像珠子般的水花。 the wave lashed against the rocks, sending up pearly spray.2.(迅猛攻击) charge; assault; dash; flewit 对社会道德观念的冲击 a shock to the sense of a community; 向敌人阵地发起冲击 charge an enemy position3.[力学] shock4.[物理学] ballistic5.[医学] ictus6.[电学] surge7.[机械工程] impact; impigement
• "冲击，冲击，冲击" 英文翻译 :    break，break，break
• "出射流" 英文翻译 :    exit flow
• "大射流" 英文翻译 :    large stream
• "氮射流" 英文翻译 :    nitrogen jet
• "多射流" 英文翻译 :    multijet
• "反射流" 英文翻译 :    reflected flux; reflex current
• "辐射流" 英文翻译 :    radial flow; radiant flux; radiation flow; radiation flux
• "回射流" 英文翻译 :    reentrant jet
• "混射流" 英文翻译 :    jet mixing flow
• "喷射流" 英文翻译 :    injection stream; injector jet; jet flow; jet stream; reaction jet; reactive jet; spraying jet; supercritical flow

• Effect of wall function in numerical study on turbulent impinging jet
  紊流冲击射流数学研究中的壁面函数法
• Numerical simulation of shock turbulence boundary layer interaction in two - dimensional nozzles
  超声速欠膨胀冲击射流的数值模拟
• Experimental investigation on noise characteristics of jets impinging on concave and convex plates
  凹凸板冲击射流噪声特性的实验研究
• When there is no impingement , the investigation about flow extravasation effect form film cooling holes is carried out with different cross flow reynolds numbers and different density flow ratios of the film outflow to cross flow
  在无冲击射流时，通过改变来流雷诺数、气膜出流与横流密流比，对气膜孔的“溢流效应”进行了研究。
• When there is impingement , the effect of flow and geometrical parameters on the local heat transfer characteristics near film cooling holes is investigated , and the mechanism of local heat transfer characteristics is obtained
  在有冲击射流时，着重研究了流动和几何参数对气膜孔局部换热特性的影响，分析了“冲击气膜出流”局部换热特性规律。
• Jet impingement cooling is an advantage method in heat transfer enhancement owing to its extremely high local heat transfer coefficient and simple structure . as regard as the combustor flame tube cooling structure is concerned , the impingement - converse convection - film composite cooling is an effective method , in this composite cooling structure , the impingement cooling problem could be modeled as impingement inside semi - confined channel
  对于冲击-逆向对流-气膜复合冷却的火焰筒结构而言,火焰筒壁面冷气侧的冲击冷却实质上是半封闭通道的冲击冷却,即冲击射流从冲击孔板喷出,冲击到换热靶面后形成壁面射流沿通道单方向流出。
• The thermal visualizations of jet impingement cooling with single or double row holes inside semi - enclosed channel are measured by using infrared camera and then the impingement cooling heat transfer coefficients are deduced . the effects of flow and geometry parameters on convective heat coefficients are obtained . the results show that : for a single row normal impingement , the impingement cooling effectiveness is enhanced with the increase of impinging reynolds number or the decrease of hole space to diameter ratio , and the best effectiveness is achieved under the jet - to - surface spacing equals to 2 ; when the jet is oblique to the confined wall , the cooling effectiveness is weaken especially under the jet - to - surface spacing ratio is greater than 2 ; for double rows normal impingement cooling , the cooling effectiveness of rear row jet is weaker than the front row under lower impinging reynolds number or bigger jet - to - surface spacing
  对于单排垂直射流,冲击冷却效果随射流雷诺数的增加、孔间距与直径比的减小而得到提高,冲击间距比为2时换热效果最好;冲击孔中心线向通道封闭一侧倾斜后,射流冲击冷却的范围变窄,当冲击间距比大于2时驻点区的对流换热能力明显降低;对于双排冲击射流,孔排间距与直径比的增加使冲击冷却范围变大,但在两排孔之间区域的对流换热系数有所下降;在较小的冲击射流雷诺数和较大的冲击间距比下,后排射流的冲击换热效果要逊于前排射流。