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Date of download: 12/18/2017 Copyright © ASME. All rights reserved.

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1 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Sketch of turbine stage housed in facility

2 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Typical turbine cooling paths

3 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Measured versus predicted Stanton number for high-pressure turbine blade

4 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Measured and predicted surface pressure (a) time history and (b) frequency content for the blade at 50% span and 6% wetted distance on suction surface

5 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Turbine stage and associated housing

6 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Cooled vane used for GE turbine stage (not to scale)

7 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Instantaneous radial velocity contours on the purge flow cavity and main gas path interface

8 Date of download: 12/18/2017 Copyright © ASME. All rights reserved. From: History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and The Ohio State University J. Turbomach. 2013;136(4): doi: / Figure Legend: Influence of tip gap on work extraction and efficiency


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