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contributor authorFernandez, Erik
contributor authorGabriel-Ohanu, Emmanuel
contributor authorVesely, Ladislav
contributor authorKapat, Jayanta
contributor authorHosangadi, Ashvin
contributor authorCooper, Paul
date accessioned2025-08-20T09:46:07Z
date available2025-08-20T09:46:07Z
date copyright4/10/2025 12:00:00 AM
date issued2025
identifier issn0742-4795
identifier othergtp_147_09_091021.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4308819
description abstractThis paper presents the second part of a study in which the leading edge and suction surface of a compressor blade was modified to delay onset of phase change for sCO2 compressors operating near the critical point. Using a first-of-its-kind apparatus for the measurement of sCO2 flow fields, Particle Image Velocimetry (PIV) is used for local flow field measurements of two compressor blade geometries: the modified “biased wedge,” and a conventional constant thickness blade. Utilizing the developed hardware, the feasibility of a simple, laser-based diagnostic for qualitatively measuring liquid phase regions, is also presented. The design of the optical diagnostics rig, a discussion of numerous challenges, and necessary considerations involved in performing optical-based measurements like PIV, in sCO2, are discussed. Velocity field measurements for the modified compressor profile show a much lower suction peak compared to a conventional blade. These results validate numerical results at the tested conditions, where the suction side profile of the biased wedge works to minimize the local pressure gradient.
publisherThe American Society of Mechanical Engineers (ASME)
titleBlade Designs for Improved Multi-Phase Performance in sCO2 Compressors: Optical Diagnostics in sCO2 and Experimental Evaluation With Particle Image Velocimetry
typeJournal Paper
journal volume147
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4066821
journal fristpage91021-1
journal lastpage91021-12
page12
treeJournal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 009
contenttypeFulltext


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