Stereoscopic PIV Measurements of the Flow Field in a Turbine Cascade

This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a ste-reoscopic particle-image velocimetry (SPIV). During the measurements, a pair of frame-straddling-based CCDcameras were configured at different sides of the laser light sheet, and appropriate tr...

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Published inJournal of thermal science Vol. 26; no. 1; pp. 89 - 95
Main Authors Tian, Yangtao, Ma, Hongwei, Ma, Rong
Format Journal Article
LanguageEnglish
Published Heidelberg Science Press 01.01.2017
Springer Nature B.V
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Abstract This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a ste-reoscopic particle-image velocimetry (SPIV). During the measurements, a pair of frame-straddling-based CCDcameras were configured at different sides of the laser light sheet, and appropriate tracing particles (DEHS) wereemployed. The measurements were conducted at the incidence angle of 0 degree and exit Reynolds number of 1.7× 10^5 with the tip clearance 1.18% of blade chord. The tip flow features, such as the evolution and breakdown oftip leakage vortex, the horseshoe vortex, turbulence characteristics of tip leakage flow, were studied for the flowfield analysis. The results showed that the tip leakage flow/vortex mainly dominate flow fields in the tip region.The tip leakage vortex performs as a concentrated vortex before its breaking down and splitting into small vortic-es. The highest turbulence intensity mainly occurs in the tip region along with the trajectory of tip leakage vortex,and when the vortex breaks down, the turbulence intensity reduces rapidly. Additionally, the SPIV with this con-figuration also shows an advantage in investigating the flow structures and mechanism inside the turbine cascade.
AbstractList This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a stereoscopic particle-image velocimetry (SPIV). During the measurements, a pair of frame-straddling-based CCD cameras were configured at different sides of the laser light sheet, and appropriate tracing particles (DEHS) were employed. The measurements were conducted at the incidence angle of 0 degree and exit Reynolds number of 1.7 × 105 with the tip clearance 1.18% of blade chord. The tip flow features, such as the evolution and breakdown of tip leakage vortex, the horseshoe vortex, turbulence characteristics of tip leakage flow, were studied for the flow field analysis. The results showed that the tip leakage flow/vortex mainly dominate flow fields in the tip region. The tip leakage vortex performs as a concentrated vortex before its breaking down and splitting into small vortices. The highest turbulence intensity mainly occurs in the tip region along with the trajectory of tip leakage vortex, and when the vortex breaks down, the turbulence intensity reduces rapidly. Additionally, the SPIV with this configuration also shows an advantage in investigating the flow structures and mechanism inside the turbine cascade.
This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a ste-reoscopic particle-image velocimetry (SPIV). During the measurements, a pair of frame-straddling-based CCDcameras were configured at different sides of the laser light sheet, and appropriate tracing particles (DEHS) wereemployed. The measurements were conducted at the incidence angle of 0 degree and exit Reynolds number of 1.7× 10^5 with the tip clearance 1.18% of blade chord. The tip flow features, such as the evolution and breakdown oftip leakage vortex, the horseshoe vortex, turbulence characteristics of tip leakage flow, were studied for the flowfield analysis. The results showed that the tip leakage flow/vortex mainly dominate flow fields in the tip region.The tip leakage vortex performs as a concentrated vortex before its breaking down and splitting into small vortic-es. The highest turbulence intensity mainly occurs in the tip region along with the trajectory of tip leakage vortex,and when the vortex breaks down, the turbulence intensity reduces rapidly. Additionally, the SPIV with this con-figuration also shows an advantage in investigating the flow structures and mechanism inside the turbine cascade.
This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a stereoscopic particle-image velocimetry (SPIV). During the measurements, a pair of frame-straddling-based CCD cameras were configured at different sides of the laser light sheet, and appropriate tracing particles (DEHS) were employed. The measurements were conducted at the incidence angle of 0 degree and exit Reynolds number of 1.7 × 10 5 with the tip clearance 1.18% of blade chord. The tip flow features, such as the evolution and breakdown of tip leakage vortex, the horseshoe vortex, turbulence characteristics of tip leakage flow, were studied for the flow field analysis. The results showed that the tip leakage flow/vortex mainly dominate flow fields in the tip region. The tip leakage vortex performs as a concentrated vortex before its breaking down and splitting into small vortices. The highest turbulence intensity mainly occurs in the tip region along with the trajectory of tip leakage vortex, and when the vortex breaks down, the turbulence intensity reduces rapidly. Additionally, the SPIV with this configuration also shows an advantage in investigating the flow structures and mechanism inside the turbine cascade.
Author TIAN Yangtao MA Hongwei MA Rong
AuthorAffiliation National Key Laboratory of Science and Technology on Aero-Engines, Collaborative Innovation Center of AdvancedAero-Engine, School of Energy & Power Engineering, Beihang University, Beijing, I00191, China
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Keywords Stereoscopic PIV
tip leakage vortex
horseshoe vortex
turbine cascade
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Snippet This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a ste-reoscopic particle-image velocimetry (SPIV). During...
This paper presents experimental measurements of the flow field in a Low-speed Turbine Cascade using a stereoscopic particle-image velocimetry (SPIV). During...
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StartPage 89
SubjectTerms cascade
Cascade flow
CCD cameras
Classical and Continuum Physics
Engineering Fluid Dynamics
Engineering Thermodynamics
Fluid dynamics
Fluid flow
Heat and Mass Transfer
horseshoe
Horseshoe vortices
Incidence angle
Leakage
Light sheets
Low speed
Particle image velocimetry
Physics
Physics and Astronomy
PIV
Reynolds number
Stereoscopic
Stereoscopy
tip
Tip clearance
turbine
Turbines
Turbulence intensity
Turbulent flow
vortex
Vortices
Title Stereoscopic PIV Measurements of the Flow Field in a Turbine Cascade
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https://link.springer.com/article/10.1007/s11630-017-0914-y
https://www.proquest.com/docview/1880797023
Volume 26
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