Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Sectional view of the test rig

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Modular setup of test configuration

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Sectional view of rotor with feed holes

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Schematics of nozzle setups

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Influence of operating conditions with dnozzle=2d0, α = 70 deg, and lNT = 30 mm

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Oil distribution for different nozzle diameters and impingement angles at V·l,in = 4 l/min

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Influence of momentum flux ratio with α = 70 deg and lNT = 30 mm

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Influence of nozzle diameter with α = 70 deg and lNT = 30 mm

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: Influence of impingement angle with lNT = 30 mm and dnozzle = d0, 1.3d0, 2d0

Date of download: 10/25/2017 Copyright © ASME. All rights reserved. From: Experimental Investigation Into the Efficiency of an Aero-engine Oil Jet Supply System J. Eng. Gas Turbines Power. 2014;137(1):011505-011505-7. doi:10.1115/1.4028255 Figure Legend: High speed images at V·l,in=6 l/min and nsh = 9000 rpm with dnozzle = 1.3d0 and lNT = 30 mm