Film cooling effectiveness is closely dependent on the geometry of the hole emitting the cooling film. These holes are sometimes quite expensive to machine by traditional methods, so 3D printed test pieces have the potential to greatly reduce the cost of film cooling experiments. What is unknown is the degree to which parameters like layer resolution and the choice among 3D printing technologies influence the results of a film cooling test. A new flat-plate film cooling facility employing oxygen-sensitive paint (OSP) verified by gas sampling and the mass transfer analogy and measurements both by gas sampling and OSP is verified by comparing measurements by both gas sampling and OSP. The same facility is then used to characterize the film cooling effectiveness of a diffuser-shaped film cooling hole geometry. These diffuser holes are then produced by a variety of additive manufacturing (AM) technologies with different build layer thicknesses. The objective is to determine if cheaper manufacturing techniques afford usable and reliable results. The coolant gas used is CO2 yielding a density ratio (DR) of 1.5. Surface quality is characterized by an optical microscope that measures surface roughness. Test coupons with rougher surface topology generally showed delayed blow off and higher film cooling effectiveness at high blowing ratios (BR) compared to the geometries with lower measured surface roughness. At the present scale, none of the additively manufactured parts consistently matched the traditionally machined part, indicating that caution should be exercised in employing additively manufactured test pieces in film cooling work.
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Research-Article
Dependence of Film Cooling Effectiveness on Three-Dimensional Printed Cooling Holes
Paul Aghasi,
Paul Aghasi
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
University of Cincinnati,
Cincinnati, OH 45221
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Ephraim Gutmark,
Ephraim Gutmark
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
University of Cincinnati,
Cincinnati, OH 45221
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David Munday
David Munday
Research Associate Professor
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
Search for other works by this author on:
Paul Aghasi
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
University of Cincinnati,
Cincinnati, OH 45221
Ephraim Gutmark
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
University of Cincinnati,
Cincinnati, OH 45221
David Munday
Research Associate Professor
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
Department of Aerospace Engineering,
University of Cincinnati,
Cincinnati, OH 45221
Contributed by the Heat Transfer Division of ASME for publication in the JOURNAL OF HEAT TRANSFER. Manuscript received September 13, 2016; final manuscript received March 27, 2017; published online June 1, 2017. Assoc. Editor: Gennady Ziskind.
J. Heat Transfer. Oct 2017, 139(10): 102003 (15 pages)
Published Online: June 1, 2017
Article history
Received:
September 13, 2016
Revised:
March 27, 2017
Citation
Aghasi, P., Gutmark, E., and Munday, D. (June 1, 2017). "Dependence of Film Cooling Effectiveness on Three-Dimensional Printed Cooling Holes." ASME. J. Heat Transfer. October 2017; 139(10): 102003. https://doi.org/10.1115/1.4036509
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