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