Heat transfer enhancement and ejection characteristics of mixing pipe with ribs for infrared suppressor

被引：0

作者：

Wu Z. ^{[1
]}

Shan Y. ^{[1
]}

Zhang J. ^{[1
]}

Yang Z. ^{[1
]}

机构：

[1] Key Laboratory of Thermal Management and Energy Utilization of Aircraft, Ministry of Industry and Information Technology, College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing

来源：

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2024年 / 50卷 / 06期

关键词：

covering shelter; ejection; heat transfer enhancement; infrared suppressor; ribs;

D O I：

10.13700/j.bh.1001-5965.2022.0548

中图分类号：

学科分类号：

摘要：

This paper proposes an enhanced heat transfer structure with ribs on the outer mixing pipe surface of the infrared suppressor in order to lower the surface temperature of the exposed covering shelter of the helicopter infrared suppressor. The ejection and heat transfer enhancement characteristics under the ribbed structure of the infrared suppressor's mixing pipe surface are studied using a numerical simulation. The results show that the ribbed mixing pipe surface convective heat transfer is enhanced by 83%, the radiation heat transfer is reduced by 31%, and the average temperature of the covering shelter surface is reduced by nearly 7 K compared with the mixing pipe surface without rib structure. The amount of second-stage induced ambient air is increased by nearly triple, and the average temperature of the covering shelter surface is reduced by nearly 18 K when the slit-inlet area on the covering shelter is increased. The hot spot on the covering shelter vanishes when the ejector airflow can directly operate on the high-temperature surface of the covering shelter after the ejection apertures at the up and down positions of the covering shelter are increased. © 2024 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.

引用

页码：2009 / 2017

页数：8

共 24 条

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