1. 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): doi: /
Figure Legend:
Sectional view of the test rig

2. 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): doi: /
Figure Legend:
Modular setup of test configuration

3. 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): doi: /
Figure Legend:
Sectional view of rotor with feed holes

4. 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): doi: /
Figure Legend:
Schematics of nozzle setups

5. 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): doi: /
Figure Legend:
Influence of operating conditions with dnozzle=2d0, α = 70 deg, and lNT = 30 mm

6. 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): doi: /
Figure Legend:
Oil distribution for different nozzle diameters and impingement angles at V·l,in = 4 l/min

7. 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): doi: /
Figure Legend:
Influence of momentum flux ratio with α = 70 deg and lNT = 30 mm

8. 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): doi: /
Figure Legend:
Influence of nozzle diameter with α = 70 deg and lNT = 30 mm

9. 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): doi: /
Figure Legend:
Influence of impingement angle with lNT = 30 mm and dnozzle = d0, 1.3d0, 2d0

10. 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): doi: /
Figure Legend:
High speed images at V·l,in=6 l/min and nsh = 9000 rpm with dnozzle = 1.3d0 and lNT = 30 mm