This paper examines the applicability of a triple layer of thermochromic liquid crystals (TLCs) for the determination of local heat transfer coefficients using the transient liquid crystal (LC) technique. The experiments were carried out in a narrow impingement channel, typically used for turbine blade cooling applications. Three types of narrow bandwidth LCs (1 °C range) of 35 °C, 38 °C, and 41 °C were individually painted on the target plate of the cooling cavity and the overall paint thickness was accurately determined with an integral coating thickness gauge. The 1D transient heat conduction equation is then implicitly solved for each individual TLC layer on its realistic depth on the painted surface. Local heat transfer coefficients are therefore calculated three times for the same location in the flow improving the measurement accuracy, especially at regions where the LC detection times are too short (stagnation points) or too long (wall-jet regions). The results indicate that if multiple LC layers are used and the paint thickness is not considered, the heat transfer coefficients can be significantly underestimated.
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February 2016
Research-Article
Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating
Alexandros Terzis,
Alexandros Terzis
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
e-mail: alexandros.terzis@me.com
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
e-mail: alexandros.terzis@me.com
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Stavros Bontitsopoulos,
Stavros Bontitsopoulos
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
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Peter Ott,
Peter Ott
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
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Jens von Wolfersdorf,
Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart,
Pfaffenwaldring 31,
Stuttgart D-70569, Germany
University of Stuttgart,
Pfaffenwaldring 31,
Stuttgart D-70569, Germany
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Anestis I. Kalfas
Anestis I. Kalfas
Laboratory of Fluid Mechanics
and Turbomachinery (LFMT),
Aristotle University of Thessaloniki (AUTH),
Thessaloniki GR-54124, Greece
and Turbomachinery (LFMT),
Aristotle University of Thessaloniki (AUTH),
Thessaloniki GR-54124, Greece
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Alexandros Terzis
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
e-mail: alexandros.terzis@me.com
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
e-mail: alexandros.terzis@me.com
Stavros Bontitsopoulos
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
Peter Ott
Group of Thermal Turbomachinery (GTT),
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
École Polytechnique Fédérale
de Lausanne (EPFL),
Lausanne CH-1015, Switzerland
Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR),
University of Stuttgart,
Pfaffenwaldring 31,
Stuttgart D-70569, Germany
University of Stuttgart,
Pfaffenwaldring 31,
Stuttgart D-70569, Germany
Anestis I. Kalfas
Laboratory of Fluid Mechanics
and Turbomachinery (LFMT),
Aristotle University of Thessaloniki (AUTH),
Thessaloniki GR-54124, Greece
and Turbomachinery (LFMT),
Aristotle University of Thessaloniki (AUTH),
Thessaloniki GR-54124, Greece
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received May 13, 2015; final manuscript received September 16, 2015; published online November 3, 2015. Assoc. Editor: Cengiz Camci.
J. Turbomach. Feb 2016, 138(2): 021003 (10 pages)
Published Online: November 3, 2015
Article history
Received:
May 13, 2015
Revised:
September 16, 2015
Citation
Terzis, A., Bontitsopoulos, S., Ott, P., von Wolfersdorf, J., and Kalfas, A. I. (November 3, 2015). "Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating." ASME. J. Turbomach. February 2016; 138(2): 021003. https://doi.org/10.1115/1.4031786
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