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压强对凸凹弯曲通道流动与传热的影响OA

Effects of pressure on flow and heat transfer in concave-convex curved channels

中文摘要英文摘要

为探究不同压强下超临界RP-3 煤油在凸凹面加热弯曲通道内的流动、传热与裂解特性,采用数值模拟方法,通过De 表征二次流强度,解释了凸凹面加热段内RP-3 煤油流动、传热与裂解特性的差异,研究了工作压强对燃料二次流速度、壁面温度与 RP-3 质量分数的影响.结果表明:在3 MPa 压强下,凸面加热段下壁耦合面附近因燃料 De 较小而出现传热恶化,壁面温度最高上升至1 409 K;凹面加热段因离心力的方向改变导致下壁耦合面附近 De 增大,壁面在 x=57.8 mm 处出现局部低温;当压强由3 MPa 提升至5 MPa,凸面加热段主流区与上壁耦合面附近的燃料De 减小,下壁耦合面附近燃料温度降低,近壁区RP-3 裂解受到抑制;凹面加热段因主流区燃料 De 受压强影响较小,近壁燃料温度始终接近裂解起始温度,RP-3 质量分数基本不变.

In order to investigate the flow,heat transfer,and pyrolysis characteristics of supercritical RP-3 kerosene in convex/concave heated curved channels under different pressures,a numerical simulation method was employed.The Dean number was used to explain the secondary flow intensity.This study clarifies the differences in the flow,heat transfer,and pyrolysis characteristics of RP-3 kerosene in the convex/concave heated sections,and examines the influence of operating pressure on the fuel secondary flow velocity,wall temperature,and RP-3 mass fraction.The results showed that under the pressure of 3 MPa,heat transfer deterioration occurred near the lower wall coupling surface in the convex heated section due to the smaller Dean number of the fuel,causing the wall temperature to rise to a maximum of 1 409 K.In the concave heated section,the change in the direction of centrifugal force led to an increase in the Dean number near the lower wall coupling surface,resulting in a local low temperature at x=57.8 mm on the wall.When the pressure increased from 3 MPa to 5 MPa,the fuel Dean number decreased in both the mainstream region and near the upper wall coupling surface of the convex heated section.Concurrently,the fuel temperature near the lower wall coupling surface decreased,which suppressed the pyrolysis of RP-3 in the near-wall region.In the concave heated section,as the fuel Dean number in the mainstream region was less affected by pressure,the near-wall fuel temperature remained close to the pyrolysis initiation temperature,and the RP-3 mass fraction remained essentially unchanged.

顾大陆;李光熙;豆飞龙;黄鋆;陈磊

西安航天动力研究所,陕西 西安 710100航天推进技术研究院,陕西 西安 710100西安航天动力研究所,陕西 西安 710100西安航天动力研究所,陕西 西安 710100西安航天动力研究所,陕西 西安 710100

航空航天

弯曲通道RP-3煤油压强传热裂解二次流

curved channelRP-3 kerosenepressureheat transferpyrolysissecondary flow

《火箭推进》 2026 (2)

94-106,13

国家自然科学基金(12345678)

10.3969/j.issn.1672-9374.2026.02.010

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