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contributor authorVega, Almudena
contributor authorCorral, Roque
date accessioned2019-02-28T11:09:58Z
date available2019-02-28T11:09:58Z
date copyright10/18/2018 12:00:00 AM
date issued2018
identifier issn0889-504X
identifier otherturbo_140_12_121007.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253373
description abstractThe dimensionless model presented in part I of the corresponding paper to describe the flutter onset of two-fin rotating seals is exploited to extract valuable engineering trends with the design parameters. The analytical expression for the nondimensional work-per-cycle depends on three dimensionless parameters of which two of them are new. These parameters are simple but interrelate the effect of the pressure ratio, the height, and length of the interfin geometry, the seal clearance, the nodal diameter (ND), the fluid swirl velocity, the vibration frequency, and the torsion center location in a compact and intricate manner. It is shown that nonrelated physical parameters can actually have an equivalent impact on seal stability. It is concluded that the pressure ratio can be stabilizing or destabilizing depending on the case, whereas the swirl of the flow is always destabilizing. Finally, a simple method to extend the model to multiple interfin cavities, neglecting the unsteady interaction among them, is described.
publisherThe American Society of Mechanical Engineers (ASME)
titleConceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation
typeJournal Paper
journal volume140
journal issue12
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4041377
journal fristpage121007
journal lastpage121007-8
treeJournal of Turbomachinery:;2018:;volume 140:;issue 012
contenttypeFulltext


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