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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 Schematic of physical phenomena in chamber Figure Legend:
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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 High-speed bearing-chamber test rig Figure Legend:
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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 Schematic showing the structure of droplet-film interaction model and the transition criteria for the various outcomes Figure Legend:
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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 Computational domain indicating the mesh density in the vicinity of the vent and scavenge ports Figure Legend:
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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 Oil droplet tracks in the vicinity of the vent port. Indicated on the plot is the roller bearing and the inlet for the sealing airflow. Figure Legend:
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Date of download: 6/29/2016 Copyright © ASME. All rights reserved. From: A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data J. Eng. Gas Turbines Power. 2004;128(1):111-117. doi:10.1115/1.1924719 Film thickness distribution on chamber housing. Arrows represent the principle directions for the interfacial shear. Figure Legend:
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