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压强对凸凹弯曲通道流动与传热的影响

顾大陆 李光熙 豆飞龙 黄鋆 陈磊

火箭推进2026,Vol.52Issue(2):94-106,13.
火箭推进2026,Vol.52Issue(2):94-106,13.DOI:10.3969/j.issn.1672-9374.2026.02.010

压强对凸凹弯曲通道流动与传热的影响

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

顾大陆 1李光熙 2豆飞龙 1黄鋆 1陈磊1

作者信息

  • 1. 西安航天动力研究所,陕西 西安 710100
  • 2. 航天推进技术研究院,陕西 西安 710100
  • 折叠

摘要

Abstract

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.

关键词

弯曲通道/RP-3煤油/压强/传热/裂解/二次流

Key words

curved channel/RP-3 kerosene/pressure/heat transfer/pyrolysis/secondary flow

分类

航空航天

引用本文复制引用

顾大陆,李光熙,豆飞龙,黄鋆,陈磊..压强对凸凹弯曲通道流动与传热的影响[J].火箭推进,2026,52(2):94-106,13.

基金项目

国家自然科学基金(12345678) (12345678)

火箭推进

1672-9374

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