1. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Schematic of compressor tip clearance casing geometry configurations

2. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Compressor measurement plane locations

3. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Compressor TPR map

4. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Change of stall conditions with tip clearance height (100% Nc)

5. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Flow range change with tip clearance height

6. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Peak total-to-static pressure rise coefficient difference as a function of tip clearance height

7. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Isentropic compressor efficiency at four corrected rotational speeds, Nc

8. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Isentropic efficiency for specified 100% Nc speedline points as a function of tip clearance height

9. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Radial stagnation pressure profiles at HL

10. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Radial stagnation pressure profiles at NS

11. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Detailed total pressure traverse measurements at stator 2 exit, axial measurement plane 6 (top), compared with qualitative flow visualization photographs of surface flows on stator 2 (bottom). Data collected at HL.

12. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Stage total-to-static pressure rise characteristics at 100% corrected speed

13. Date of download: 11/12/2017
Copyright © ASME. All rights reserved.
From: The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications
J. Eng. Gas Turbines Power. 2015;138(5): doi: /
Figure Legend:
Comparison of rotor and stage efficiency differences with tip clearance height at NL and HL