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A NOVEL MICROELECTRONICS COOLING TECHNIQUE USING A PAIR OF UNSTEADY CONFINED IMPINGING AIR JETS

机译:一种新的微电子冷却技术,使用一对不稳定的撞击撞击空气喷气机

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The unsteady laminar flow and heat transfer characteristics for a pair of confined impinging air jets centered in a channel were studied numerically. The time-averaged heat transfer coefficient for a pair of heat sources centered in the channel and aligned with the jets was determined as well as the oscillating jet frequency for the unsteady cases. The present study continues the authors' previous investigation, which emphasized how single confined jets will remain steady at Reynolds numbers that make side-by-side jets highly unsteady. The nature of this unsteadiness depends on the proximity of the jet inlets, the channel dimensions and the jet Reynolds number. The jet unsteadiness causes the stagnation point locations to sweep back and forth over the impingement region, and the jets "wash" a larger surface area on the target wall. The results indicate that the dual jets become unsteady between a Reynolds number of 200 and 300. Also, in the range of Reynolds numbers studied, a fixed stagnation "bubble" was formed on the target wall between the two jets, which reduced the heat transfer removal from that region, leading in fact to a quasi-independence of the local heat transfer on flow conditions. The stagnant region contains slow moving warm air that forces the cool impinging air jets to flow to the sides of this target wall area. The oscillating frequency of the flow increases with Reynolds number for the unsteady cases. Also, the time-averaged heat transfer coefficient on the heat sources rises as the Reynolds number increases for the steady cases but there is a slight decrease when it transitions to unsteady flow, indicating again that the stagnation "bubble" occurring between the two heat sources affects the local heat transfer.
机译:在数值上研究了一对狭窄的撞击空气喷射的不稳定层流和传热特性。确定在通道中并与喷射器对准的一对热源的时间平均传热系数,以及不稳定情况的振荡射流。本研究继续提交的先前调查,这强调了单一限制喷气机如何在雷诺数的雷诺数仍然稳定,使其并排射流高度不稳定。这种不稳定性的性质取决于喷射入口,通道尺寸和喷射雷诺数的接近度。喷射不稳定性导致停滞点位置在冲击区域上来回扫过,并且喷射器“清洗”靶壁上的较大表面积。结果表明,双喷射在雷诺数200和300之间变得不稳定。此外,在所研究的雷诺数的范围内,在两个喷射器之间的靶壁上形成固定停滞“气泡”,这减少了传热从该地区移除,实际上导致局部传热对流动条件的准独立性。停滞区域含有缓慢移动的暖空气,其迫使冷却的撞击空气喷射流到该目标壁区域的侧面。流量的振荡频率随着不稳定情况的雷诺数而增加。此外,随着恢复速度的增加,热源上的时间平均传热系数升高,但在稳定情况下增加时,当它转变为不稳定的流量时,再次表明两个热源之间发生的停滞“气泡”的滞后性“气泡”。影响局部传热。

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