摘要
通过地面离心转台模拟过载,对R134a在内径为1.002mm管内的沸腾流动传热进行了实验研究。结果表明:管内流动沸腾传热特性随着重力的变化而变化;在重力为3.16g(g=9.8m/s^2)时,过载下的传热系数比常重力下的大;随着过载的增加,大多数情况下传热系数先增大后减小,转折点在1.1g^1.4g;在3.16g时,部分传热系数开始出现低于1g时的情况;干度对传热系数的影响特性因重力不同而不同。研究了常重力下流动沸腾预测模型对过载环境的适应性,鉴别出了对过载数据预测较好的公式。
An experiment investigation of R134 aflow boiling heat transfer in a 1.002 inner diameter mini-tube under hypergravity was carried out,with the hypergravity environment being achieved using a centrifugal acceleration machine.Results showed that a remarkable difference existed in flow boiling heat transfer between hypergravity and normal gravity.The heat transfer under hypergravity was stronger than that under normal gravity in the gravity of 3.16 g(g=9.8 m/s^2).With the increase of gravity,heat transfer coefficients increased at first and then decreased.The transition took place around 1.1 g-1.4 g.At3.16 g,some heat transfer coefficients became smaller than those at normal gravity.The effects of vapor quality on the heat transfer varied with gravity.The applicability of correlations for flow boiling heat transfer under normal gravity to hypergravity was also evaluated,and those having good prediction performances for hypergravity were identified.
作者
方贤德
李国华
袁宇良
李定坤
郑玲
FANG Xiande;LI Guohua;YUAN Yuliang;LI Dingkun;ZHENG Ling(Key Laboratory of Aircraft Environment Control and Life Support,Ministry of Industry and Information Technolgy,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2019年第8期1644-1651,共8页
Journal of Aerospace Power
基金
国家自然科学基金(51576099,51176074)
江苏高校优势学科建设工程资助项目
关键词
过载
气液两相流
流动沸腾
传热
细小通道
hypergravity
gas-liquid two-phase flow
flow boiling
heat transfer
mini-channel