微重力下高热流时池内双组分核态沸腾  

NUCLEATE BOILING OF BINARY MIXTURE AT HIGH HEAT FLUX UNDER MICROGRAVITY

作　　者：柴立和[1] 彭晓峰[1] 

机构地区：[1]清华大学

出　　处：《航空动力学报》1998年第3期263-266,共4页Journal of Aerospace Power

基　　金：国家自然科学基金;国家教委优秀年轻教师基金

摘　　要：本文基于Ｈｅｌｍｈｏｌｔｚ不稳定性原理建立了微重力下双组分高热流时核态沸腾的双层汽泡结构模型。由于浮力很小，这种结构能维持到ＣＨＦ状态。通过对该结构的深入分析，导得了汽柱面积占总面积的百分比及液体层初始厚度的表达式，在此基础上发展了ＣＨＦ模型。分析结果同实验结果及地面条件下的结果作了比较，对异同之处作出了合理的解释。An analytical model for nucleate pool boiling heat transfer of binary mixtures in high-flux regime is formulated according to Helmholtz instability theory of vapor-liquid interface.The nucleate pool boiling for binary mixtures at high heat flux under microgravity is also characterized by the existence of a liquid layer known as macrolayer between the heater surface and the vapor mass.The dual bubble layer structure can maintain up to CHF condition due to less buoyancy.The expressions for fraction of bubble contact area on the heater surface and initial macrolayer thickness are derived in term of the thermophysical properties or/and the heat flux.A CHF model based on hydrodynamics is provided.The predicted results are compared with experimental data and theoretical analysis.Some important conclusions are drawn as follows:The fraction of bubble contact area on the heater surface is independent of the input heat flux,but much greater than that at terrestrial conditions;Initial macrolayer thickness is much greater than that at terrestrial conditions due to less velocities of vapor phase and liquid phase;The CHF values for binary mixtures under microgravity are about 60～80% of those at terrestrial conditions,but are much greater than those of single components under microgravity.

关 键 词：传热 沸腾 汽泡动力学 航天器 换热设备 微重力 

分 类 号：V419.2[航空宇航科学与技术—航空宇航推进理论与工程] V423