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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Schematic of compressor tip clearance casing geometry configurations

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Compressor measurement plane locations

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Compressor TPR map

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Change of stall conditions with tip clearance height (100% Nc)

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Flow range change with tip clearance height

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Peak total-to-static pressure rise coefficient difference as a function of tip clearance height

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Isentropic compressor efficiency at four corrected rotational speeds, Nc

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Isentropic efficiency for specified 100% Nc speedline points as a function of tip clearance height

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Radial stagnation pressure profiles at HL

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Radial stagnation pressure profiles at NS

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):052605-052605-10. doi:10.1115/1.4031625 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.

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Stage total-to-static pressure rise characteristics at 100% corrected speed

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):052605-052605-10. doi:10.1115/1.4031625 Figure Legend: Comparison of rotor and stage efficiency differences with tip clearance height at NL and HL