A novel heat flux sensor was tested that allows for time-resolved heat flux measurements in internal ribbed channels related to the study of passages in gas turbine blades. The working principle of the atomic layer thermopile (ALTP) sensor is based on a thermoelectric field created by a temperature gradient over an yttrium-barium-copper-oxide (YBCO) crystal (the transverse Seebeck effect). The sensors very fast frequency response allows for highly time-resolved heat flux measurements up to the range. This paper explains the design and working principle of the sensor, as well as the benchmarking of the sensor for several flow conditions. For internal cooling passages, this novel sensor allows for highly accurate, time-resolved measurements of heat transfer coefficients, leading to a greater understanding of the influence of fluctuations in temperature fields.
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e-mail: roediger@iag.uni-stuttgart.de
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January 2008
Research Papers
Time-Resolved Heat Transfer Measurements on the Tip Wall of a Ribbed Channel Using a Novel Heat Flux Sensor—Part I: Sensor and Benchmarks
Tim Roediger,
Tim Roediger
Institute of Aerodynamics and Gas Dynamics (IAG),
e-mail: roediger@iag.uni-stuttgart.de
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
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Helmut Knauss,
Helmut Knauss
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
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Uwe Gaisbauer,
Uwe Gaisbauer
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
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Ewald Kraemer,
Ewald Kraemer
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
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Sean Jenkins,
Sean Jenkins
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart
, Pfaffenwaldring 31, Stuttgart, Germany 70569
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Jens von Wolfersdorf
Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart
, Pfaffenwaldring 31, Stuttgart, Germany 70569
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Tim Roediger
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569e-mail: roediger@iag.uni-stuttgart.de
Helmut Knauss
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
Uwe Gaisbauer
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
Ewald Kraemer
Institute of Aerodynamics and Gas Dynamics (IAG),
University of Stuttgart
, Pfaffenwaldring 21, Stuttgart, Germany 70569
Sean Jenkins
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart
, Pfaffenwaldring 31, Stuttgart, Germany 70569
Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart
, Pfaffenwaldring 31, Stuttgart, Germany 70569J. Turbomach. Jan 2008, 130(1): 011018 (8 pages)
Published Online: January 28, 2008
Article history
Received:
July 17, 2006
Revised:
September 25, 2006
Published:
January 28, 2008
Citation
Roediger, T., Knauss, H., Gaisbauer, U., Kraemer, E., Jenkins, S., and von Wolfersdorf, J. (January 28, 2008). "Time-Resolved Heat Transfer Measurements on the Tip Wall of a Ribbed Channel Using a Novel Heat Flux Sensor—Part I: Sensor and Benchmarks." ASME. J. Turbomach. January 2008; 130(1): 011018. https://doi.org/10.1115/1.2751141
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