首页> 外文会议>International conference on nanochannels, microchannels and minichannels;ICNMM2011 >EXPERIMENTAL INVESTIGATIONS OF LAMINAR, TRANSITIONAL TO TURBULENT GAS FLOW IN RIB-PATTERNED MICRO-CHANNELS
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EXPERIMENTAL INVESTIGATIONS OF LAMINAR, TRANSITIONAL TO TURBULENT GAS FLOW IN RIB-PATTERNED MICRO-CHANNELS

机译:肋式微通道内层流,过渡到湍流气流的实验研究

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The effects of rib-patterned surfaces on laminar, transitional to turbulent gas flow in micro-channels were experimentally investigated in the present study. The experiments were performed for two micro-channels having either smooth or rib-patterned surfaces. The micro-channels were etched into silicon wafers and capped with glass substrates. The micro-ribs were patterned on the micro-channel surfaces and oriented perpendicular to the flow direction. The pressure was measured at seven locations along the channel length to determine local values of Mach number and friction factor for a wide range of flow regime from laminar to turtmlent flow. The friction factors with the hydraulic diameter based on the rib-to-upper-wall height were compared with that for incompressible theory on Moody chart. The values of the product of friction factor and Reynolds number (f·Re) as a function of Mach number were also compared with those of smooth micro-channels and incompressible theory.
机译:在本研究中,通过实验研究了肋状图案表面对微通道中层流,过渡到湍流气流的影响。对具有光滑或肋状图案表面的两个微通道进行了实验。将微通道蚀刻到硅晶片中,并盖上玻璃基板。将微肋在微通道表面上构图并垂直于流向定向。在沿通道长度的七个位置测量压力,以确定从层流到湍流的各种流动状态的马赫数和摩擦系数的局部值。将水力直径基于肋骨至上壁高度的摩擦因数与穆迪图上不可压缩理论的摩擦因数进行了比较。还将摩擦因数和雷诺数(f·Re)乘积与马赫数的函数值与光滑微通道和不可压缩理论的值进行了比较。

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