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contributor authorInman, Daniel
contributor authorCuadrado, David G.
contributor authorAndreoli, Valeria
contributor authorFisher, Jordan
contributor authorPaniagua, Guillermo
contributor authorAye-Addo, Papa Aye N.
contributor authorBhatnagar, Lakshya
contributor authorLozano, Francisco
contributor authorMeyer, Terrence
contributor authorBloxham, Matthew
date accessioned2022-02-05T22:23:32Z
date available2022-02-05T22:23:32Z
date copyright3/31/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_143_06_061031.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277454
description abstractParticle image velocimetry (PIV) is a well-established technique for determining the flow direction and velocity magnitude of complex flows. This paper presents a methodology for executing this nonintrusive measurement technique to study a scaled-up turbine vane geometry within an annular cascade at engine-relevant conditions. Custom optical tools such as laser delivery probes and imaging inserts were manufactured to mitigate the difficult optical access of the test section and perform planar PIV. With the use of a burst-mode Nd: YAG laser and Photron FASTCAM camera, the frame straddling technique is implemented to enable short time intervals for the collection of image pairs and velocity fields at 10 kHz. Furthermore, custom image processing tools were developed to optimize the contrast and intensity balance of each image pair to maximize particle number and uniformity while removing scattering and background noise. The preprocessing strategies significantly improve the vector yield under challenging alignment, seeding, and illumination conditions. With the optical and software tools developed, planar PIV was conducted in the passage of a high-pressure stator row, at midspan, in an annular cascade. Different Mach and Reynolds number operating conditions were achieved by modifying the temperature and mass flow. With careful spatial calibration, the resultant velocity vector fields are compared with Reynolds-averaged-Navier–Stokes (RANS) simulations of the vane passage with the same geometry and flow conditions. Uncertainty analysis of the experimental results is also presented and discussed, along with prospects for further improvements.
publisherThe American Society of Mechanical Engineers (ASME)
titleParticle Image Velocimetry in a High-Pressure Turbine Stage at Aerodynamically Engine Representative Conditions
typeJournal Paper
journal volume143
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4049448
journal fristpage061031-1
journal lastpage061031-10
page10
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 006
contenttypeFulltext


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