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contributor authorBraun, James
contributor authorPaniagua, Guillermo
contributor authorFalempin, Francois
contributor authorLe Naour, Bruno
date accessioned2022-02-04T14:41:41Z
date available2022-02-04T14:41:41Z
date copyright2020/02/14/
date issued2020
identifier issn0742-4795
identifier othergtp_142_04_041024.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274179
description abstractSupersonic inlet flow is usually considered to be detrimental to the performance of turbine systems. A new class of bladeless turbines was developed, which allows for power extraction from supersonic axial inflows without swirl with minimal maintenance cost. This is achieved through a wavy hub surface that promotes shocks and expansion fans and hence generates torque. In a first step, a baseline bladeless turbine is designed and the power extraction is analyzed. The bladeless turbine surface is parametrized in matlab and subsequently imported into Hexpress (Numeca) to mesh an unstructured grid. The first layer thickness is kept below one for all the simulations. The unstructured mesh is loaded into cfd++ (Metacomp) to solve the three dimensional steady Reynolds-averaged Navier–Stokes (RANS) equations. Second, the work extraction principle is broken down from a three-dimensional unsteady problem into a two-dimensional steady phenomenon. An experimental campaign is outlined and test details are discussed. Finally, after the experimental characterization, the operational envelope and scaling of the bladeless turbine are described for several reduced mass flows, reduced speeds, and geometrical features of the turbine (amplitude of the wavy surface, helix angle, hub radius, and length of the axial turbine).
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign and Experimental Assessment of Bladeless Turbines for Axial Inlet Supersonic Flows
typeJournal Paper
journal volume142
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4045359
page41024
treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 004
contenttypeFulltext


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