中国航空学报(英文版)2024,Vol.37Issue(3) :7-20.DOI:10.1016/j.cja.2023.10.006

Tomographic particle image velocimetry measurement on three-dimensional swirling flow in dual-stage counter-rotating swirler

Yuyang ZHOU Ling DONG Mingtao SHANG Jibao LI Akira RINOSHIKA
中国航空学报(英文版)2024,Vol.37Issue(3) :7-20.DOI:10.1016/j.cja.2023.10.006

Tomographic particle image velocimetry measurement on three-dimensional swirling flow in dual-stage counter-rotating swirler

Yuyang ZHOU 1Ling DONG 2Mingtao SHANG 3Jibao LI 3Akira RINOSHIKA4
扫码查看

作者信息

  • 1. Key Laboratory of Fluid Mechanics of Ministry of Education,Beihang University,Beijing 100191,China
  • 2. School of Mechanical and Automotive Engineering,Shanghai University of Engineering Science,Shanghai 201620,China
  • 3. AECC Commercial Aircraft Engine Co.,Ltd.,Shanghai 200241,China
  • 4. Department of Mechanical Systems Engineering,Yamagata University,Yamagata 992-8510,Japan
  • 折叠

Abstract

Three-Dimensional(3D)swirling flow structures,generated by a counter-rotating dual-stage swirler in a confined chamber with a confinement ratio of 1.53,were experimentally investi-gated at Re=2.3 × 105 using Tomographic Particle Image Velocimetry(Tomo-PIV)and planar Particle Image Velocimetry(PIV).Based on the analysis of the 3D time-averaged swirling flow structures and 3D Proper Orthogonal Decomposition(POD)of the Tomo-PIV data,typical coher-ent flow structures,including the Corner Recirculation Zone(CRZ),Central Recirculation Zone(CTRZ),and Lip Recirculation Zone(LRZ),were extracted.The counter-rotating dual-stage swir-ler with a Venturi flare generates the independence process of vortex breakdown from the main stage and pilot stage,leading to the formation of an LRZ and a smaller CTRZ near the nozzle out-let.The confinement squeezes the CRZ to the corner and causes a reverse rotation flow to limit the shape of the CTRZ.A large-scale flow structure caused by the main stage features an explosive breakup,flapping,and Precessing Vortex Core(PVC).The explosive breakup mode dominates the swirling flow structures owing to the expansion and construction of the main jet,whereas the flapping mode is related to the wake perturbation.Confinement limits the expansion of PVC and causes it to contract after the impacting area.

Key words

Coherent structures/Dual-stage counter-rotating swirler cup/Precessing vortex core/Proper orthogonal decom-position/Swirling flow/Tomographic particle image velocimetry

引用本文复制引用

基金项目

国家自然科学基金(12232002)

国家自然科学基金(12072017)

国家自然科学基金(12002199)

国家自然科学基金(11721202)

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)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量37
段落导航相关论文