超临界压力甲烷异常传热行为的机理研究

本文对水平管道内超临界压力下甲烷的流动与传热过程进行了数值模拟,得到了5MPa下质量流率范围为200~400 kg/(m^2·s),热流密度范围为100~400 kW/m^2工况下的传热规律。提出了以热质比r(热流密度与质量流率的比值)为判据来预测异常传热行为(传热强化和传热恶化相继发生):在r>0.5 kJ/kg工况下,传热出现异常行为;在r≤0.5 kJ/kg工况范围内,异常传热行为消失,换热系数沿程呈下降趋势。在此基础上,对典型传热工况进行了深入的机理分析。结果表明:二次环流涡心的偏移是传热异常的主要原因,环流涡心向管壁偏移可使边界层减薄从而强化传热,环流涡心向轴线偏移则使边界层增厚、发生"湍流层流化",从而恶化传热;湍动能的增大是换热系数增大、换热进入恢复区的主要原因,随着二次环流减弱换热进入正常传热阶段。

超临界压力甲烷异常传热行为的机理研究

本文对水平管道内超临界压力下甲烷的流动与传热过程进行了数值模拟,得到了5 MPa下质量流率范围为200~400 kg/(m^2·s),热流密度范围为100~400 kW/m^2工况下的传热规律。提出了以热质比r(热流密度与质量流率的比值)为判据来预测异常传热行为(传热强化和传热恶化相继发生):在r>0.5 kJ/kg工况下,传热出现异常行为;在r≤0.5 kJ/kg工况范围内,异常传热行为消失,换热系数沿程呈下降趋势。在此基础上,对典型传热工况进行了深入的机理分析。结果表明:二次环流涡心的偏移是传热异常的主要原因,环流涡心向管壁偏移可使边界层减薄从而强化传热,环流涡心向轴线偏移则使边界层增厚、发生“湍流层流化”,从而恶化传热;湍动能的增大是换热系数增大、换热进入恢复区的主要原因,随着二次环流减弱换热进入正常传热阶段。

Experimental study of a supersonic turbulent boundary layer using PIV

Particle image velocimetry was applied to the study of the statistical properties and the coherent structures of a fiat plate turbulent boundary layer at Mach 3. The nanoparticles with a good flow-following capability in supersonic flows were adopted as the tracer particles in the present experiments. The results show that the Van Driest transformed mean velocity profile satisfies the incompressible scalings and reveals a log-law region that extends to yld=0.4, which is further away from the wall than that in incompressible boundary layers. The Reynolds stress profiles exhibit a plateau-like region in the log-law region. The hairpin vortices in the streamwise-wall-normal plane are identified using different velocity decompositions, which are similar to the results of the flow visualization via NPLS technique. And multiple hairpin vortices are found moving at nearly the same velocity in different regions of the boundary layer. In the streamwise-spanwise plane, elongated streaky structures are observed in the log-law region, and disappear in the outer region of the boundary layer, which is contrary to the flow visualization results.