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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Sketch of turbine stage housed in facility
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Typical turbine cooling paths
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Measured versus predicted Stanton number for high-pressure turbine blade
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):041004-041004-11. doi:10.1115/1.4024898 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
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Turbine stage and associated housing
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Cooled vane used for GE turbine stage (not to scale)
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Instantaneous radial velocity contours on the purge flow cavity and main gas path interface
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):041004-041004-11. doi:10.1115/1.4024898 Figure Legend: Influence of tip gap on work extraction and efficiency