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contributor authorBenzon, D.
contributor author½idonis, A.
contributor authorPanagiotopoulos, A.
contributor authorAggidis, G. A.
contributor authorAnagnostopoulos, J. S.
contributor authorPapantonis, D. E.
date accessioned2017-05-09T01:18:52Z
date available2017-05-09T01:18:52Z
date issued2015
identifier issn0098-2202
identifier otherfe_137_04_041106.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158225
description abstractThis study utilizes two modern computational fluid dynamics (CFD) software packages (ansysآ®cfxآ® and ansysآ®fluentآ®) to analyze the basic geometric factors affecting the efficiency of a typical impulse turbine injector. A design of experiments (DOEs) study is used to look at the impact of four primary nozzle and spear design parameters on the injector losses over a range of inlet pressures. Improved injector designs for both solvers are suggested based on the results and comparisons are made. The results for both CFD tools suggest that steeper injector nozzle and spear angles than current literature describes will reduce the losses by up to 0.6%.
publisherThe American Society of Mechanical Engineers (ASME)
titleImpulse Turbine Injector Design Improvement Using Computational Fluid Dynamics
typeJournal Paper
journal volume137
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4029310
journal fristpage41106
journal lastpage41106
identifier eissn1528-901X
treeJournal of Fluids Engineering:;2015:;volume( 137 ):;issue: 004
contenttypeFulltext


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