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): doi: / Schematic of physical phenomena in chamber Figure Legend:

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): doi: / High-speed bearing-chamber test rig Figure Legend:

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): doi: / Schematic showing the structure of droplet-film interaction model and the transition criteria for the various outcomes Figure Legend:

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): doi: / Computational domain indicating the mesh density in the vicinity of the vent and scavenge ports Figure Legend:

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): doi: / 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:

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): doi: / Film thickness distribution on chamber housing. Arrows represent the principle directions for the interfacial shear. Figure Legend: