Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure.

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Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Cross section (left) and rear view (right) of the high speed bar rotating rig Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Hot wire calibration map Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Nondimensional KSI against Mach number. Steady and unsteady inflow. Re3=1.3×105. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Isentropic blade surface Mach number distributions. Steady inflow. Re3=1.3×105. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Nondimensional KSI against Mach number. Steady and unsteady inflow. Re3=2.0×105. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Contours of ensemble averaged velocity on smooth surface (top) and with the trip at 60%S0 (bottom). Steady inflow. M3=0.61, Re3=1.3×105. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Shape factor at different snapshots for the cases of a smooth surface and trip at 60%S0. M3=0.61, Re3=1.3×105. fr=0.48. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Contours of time mean velocity on smooth surface (top) and with the trip at 66%S0 (center) and with the trip at 60%S0 (bottom). Steady inflow. M3=0.74, Re3=1.3×105. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / rms of the unsteady pressure measurements as fractions of the exit dynamic pressure. Re3=1.3×105. Steady inflow. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Ensemble averaged unsteady pressure, raw pressure and rms as fractions of the exit dynamic pressure. M3=0.61, Re3=1.3×105. Streamwise location 85%S0. Unsteady inflow, fr=0.48. Figure Legend:

Date of download: 5/31/2016 Copyright © ASME. All rights reserved. From: The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade J. Turbomach. 2004;127(4): doi: / Unsteady ensemble averaged pressure (top) and rms as a fraction of exit dynamic pressure (bottom) for the case of smooth surface and trip at 60%S0. M3=0.74, Re3=1.3×105. Streamwise location 85%S0. Unsteady inflow, fr=0.40. Figure Legend: