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Labyrinth seals are the simple and most commonly used rotating seal in cold (compressor) and hot (turbine) regions of gas turbine engines. In order to achieve successful engine design estimating accurate leakage flow rates, windage heating and heat transfer coefficients are critical for rotor dynamic stability. The windage effect inside the flow creates direct loss of power also increase fluid temperature. In this paper numerical simulation of a canted stepped labyrinth seal is performed using commercial Fluent CFD code with 2D axisymmetric is used to study leakage flow and windage heating for various seal clearances for solid (smooth) stator land geometry. The 2D model is subsequently used to determine average heat transfer coefficients on the rotor and stator for heating and cooling situations.
Mohana Rao. 2018. "Leakage and Thermal Characterisation of Canted Labyrinth Seals". Global Journal of Research in Engineering, Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 17 (GJRE Volume 17 Issue A7).
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
v1.2
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Total Score: 107
Country: India
Subject: Global Journal of Research in Engineering
Authors: Mohana Rao, Dr. Manzoor Husain (PhD/Dr. count: 1)
View Count (all-time): 370
Total Views (Real + Logic): 1484
Total Downloads (simulated): 93
Publish Date: 2017 01, Sun
Monthly Totals (Real + Logic):
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