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TR-1A rocket experiment on nucleate pool boiling heat transfer under microgravity

机译:TR-1A火箭试验在微匍匐下核心池沸腾的热传递

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To clarify the reason of inconsistent trends in the existing heat transfer data in microgravity nucleate boiling, the method to acquire the local heat transfer data and to observe in detail the bubble behavior from underneath was developed andintroduced in the experiment by the use of the NASDA TR-1A ballistic rocket. The pool boiling experiment was conducted using ethanol as test liquid at an almost constant temperature of 25 to 30°C. The system pressure was varied from 0.01 to 0.48 MPa withcorresponding liquid subcooling from 3 to 95 K. The steady state heat transfer is realized in microgravity at the conditions of moderate and high subcooling where the bubble size is determined so that the rate of evaporation of microlayer balances that of condensation at the bubble surface. On the other hand, the transition to burnout is unavoidable even at low heat flux when the liquid of low subcooling is concerned. The nucleate boiling heat transfer is dominated by the isolated or primary bubbles justgenerated on the heat transfer surface even in the high heat flux or the low liquid subcooling region where these bubbles lift the large coalesced one covering the entire heating surface. Two opposite trends of the heat transfer enhancement anddeterioration are possible depending on the behavior of dry patches extending in the microlayer underneath the bubbles contacting directly with the surface.
机译:为了澄清在微肉体核心沸腾中现有的传热数据中存在不一致趋势的原因,该方法获取局部传热数据并详细观察下面的泡沫行为在实验中通过使用NASDA TR在实验中发育-1a弹道火箭。使用乙醇作为测试液在25至30℃的几乎恒定温度下使用乙醇进行池沸腾实验。系统压力从0.01至0.48MPa的再生液过冷却,从3至95k变化。在测定气泡尺寸的中等和高级冷却条件下,在微匍匐情况下实现稳态热转移,从而确定微层的蒸发速率。微层的蒸发速率平衡气泡表面冷凝的余地。另一方面,当涉及低过脱机的液体时,即使在低热量通量下也是不可避免的倦怠的过渡。即使在高热通量或低液体过冷区域中,核心沸腾的传热由刚刚被隔离的或主要气泡的分离的或主要气泡占据在热传递表面上,或者在高热通量或低液体过冷区域上,这些气泡抬起大型聚结的覆盖整个加热表面。根据在直接与表面直接接触的气泡下方的微层中延伸的干贴片的行为,可以实现热传递增强频道的两个相反趋势。

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