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

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

扫码查看
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.

Coherent structuresDual-stage counter-rotating swirler cupPrecessing vortex coreProper orthogonal decom-positionSwirling flowTomographic particle image velocimetry

Yuyang ZHOU、Ling DONG、Mingtao SHANG、Jibao LI、Akira RINOSHIKA

展开 >

Key Laboratory of Fluid Mechanics of Ministry of Education,Beihang University,Beijing 100191,China

School of Mechanical and Automotive Engineering,Shanghai University of Engineering Science,Shanghai 201620,China

AECC Commercial Aircraft Engine Co.,Ltd.,Shanghai 200241,China

Department of Mechanical Systems Engineering,Yamagata University,Yamagata 992-8510,Japan

展开 >

国家自然科学基金国家自然科学基金国家自然科学基金国家自然科学基金

12232002120720171200219911721202

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
年,卷(期):2024.37(3)
  • 37