All experimental technique has been developed for measurement of local convection heat transfer characteristics on rotating surfaces, utilizing thin liquid crystal surface coatings in a thermal transient test procedure. The encapsulated liquid crystal coatings used are sprayed directly on the test surface and their response is observed and processed during the transient with automated computer vision and data acquisition systems. Heat transfer coefficients are calculated from the thermal transient response of the test surface, as determined from the color indication from the thin coating. A significant advantage of the method, especially for convection in disk/shroud cavities that may contain recirculating fluid regions, is that appropriate thermal boundary conditions are naturally imposed on all of the boundary surfaces. The method is also relatively fast and inexpensive, and allows the geometry of the disk and stator surfaces to be changed easily, without the expenses of mounting discrete heat flux and temperature sensors and equipment to transfer information to a stationary frame of reference. Application of the experimental technique is demonstrated with detailed radially local surface Nusselt number distributions acquired for cases involving jet impingement onto a plane smooth disk, rotating in close proximity to a parallel plane stator disk. A single circular jet, with nozzle exit flush mounted in the stator, is oriented normal to the disk surface at various radii and flowrates. Local Nusselt numbers are presented nondimensionally as functions of both disk and flow Reynolds numbers. The results indicate that the local radial heat transfer distribution can be controlled by varying the impingement radius, but maximum radially averaged heat transfer is obtained with impingement at the disk center.
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ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
June 4–8, 1989
Toronto, Ontario, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7916-0
PROCEEDINGS PAPER
Transient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement
D. E. Metzger,
D. E. Metzger
Arizona State University, Tempe, AZ
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R. S. Bunker,
R. S. Bunker
Arizona State University, Tempe, AZ
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G. Bosch
G. Bosch
Arizona State University, Tempe, AZ
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D. E. Metzger
Arizona State University, Tempe, AZ
R. S. Bunker
Arizona State University, Tempe, AZ
G. Bosch
Arizona State University, Tempe, AZ
Paper No:
89-GT-287, V004T08A032; 8 pages
Published Online:
March 18, 2015
Citation
Metzger, DE, Bunker, RS, & Bosch, G. "Transient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement." Proceedings of the ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition. Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration. Toronto, Ontario, Canada. June 4–8, 1989. V004T08A032. ASME. https://doi.org/10.1115/89-GT-287
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