中国航空学报(英文版)2024,Vol.37Issue(5) :180-198.DOI:10.1016/j.cja.2024.01.027

Numerical study of steady flow characteristics of a rear variable-area bypass injector with alternating area regulator

Runfu LIU Zhenyao LI Huiliu ZHANG Qixing WANG Yue HUANG Yancheng YOU
中国航空学报(英文版)2024,Vol.37Issue(5) :180-198.DOI:10.1016/j.cja.2024.01.027

Numerical study of steady flow characteristics of a rear variable-area bypass injector with alternating area regulator

Runfu LIU 1Zhenyao LI 1Huiliu ZHANG 1Qixing WANG 1Yue HUANG 1Yancheng YOU1
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作者信息

  • 1. School of Aerospace Engineering,Xiamen University,Xiamen 361000,China
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Abstract

The mixing effectiveness of the airflow between the inner and outer bypass inlets of a Rear Variable-Area Bypass Injector(RVABI)is the key to the afterburner performance of variable cycle engines.This paper describes an optimized RVABI design based on an alternating area reg-ulator to improve the velocity/temperature uniformity of the incoming flow at the afterburner.Compared with a classical RVABI,numerical simulations show that the proposed alternating RVABI performs better in terms of thermal mixing efficiency and total pressure loss in different variable cycle engine modes.Both the increasing air contact area between the inner and outer bypass of alternating structure RVABI,and a larger streamwise vortex in the inner bypass inlet due to the proposed alternating lobe structure in the RVABI contribute to the significantly increase of mixing effectiveness.Besides,the alternating regulator induces strong streamwise vortex,which helps to improve the airflow mixing with its vortex-induced velocity.The interaction between the streamwise vortex and azimuthal vortex further promises the velocity/temperature uniformity after the RVABI.With the increase of alternating lobe's height ratio,the covering area of the streamwise vortex and the azimuthal vortex is enlarged,which further enhances the thermal mixing efficiency of the RVABI.This design gives an insight into the future design and optimization of RVABI.

Key words

Alternating area regulator/Lobed mixer/Variable cycle engine/Rear Variable-Area Bypass Injector(RVABI)/Streamwise vortex

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基金项目

National Science and Technology Major Project,China(J2019-Ⅲ-0016-0060)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDCSCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量30
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