A special naphthalene sublimation technique is used to study the film cooling performance downstream of one row of holes of 35 deg inclination angle with 3d hole spacing and relatively small hole length to diameter ratio (L/d = 6.3). Both film cooling effectiveness and mass/heat transfer coefficient are determined for blowing rates from 0.5 to 2.0 with density ratio of 1.0. The mass transfer coefficient is measured using pure air film injection, while the film cooling effectiveness is derived from comparison of mass transfer coefficients obtained following injection of naphthalene-vapor-saturated air with those from pure air injection. This technique enables one to obtain detailed local information on film cooling performance. The laterally averaged and local film cooling effectiveness agree with previous experiments. The difference between mass/heat transfer coefficients and previous heat transfer results indicates that conduction error may play an important role in the earlier heat transfer measurements.
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April 1999
Research Papers
Film Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes
R. J. Goldstein,
R. J. Goldstein
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
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P. Jin,
P. Jin
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
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R. L. Olson
R. L. Olson
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
Search for other works by this author on:
R. J. Goldstein
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
P. Jin
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
R. L. Olson
Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455
J. Turbomach. Apr 1999, 121(2): 225-232 (8 pages)
Published Online: April 1, 1999
Article history
Received:
February 1, 1998
Online:
January 29, 2008
Citation
Goldstein, R. J., Jin, P., and Olson, R. L. (April 1, 1999). "Film Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes." ASME. J. Turbomach. April 1999; 121(2): 225–232. https://doi.org/10.1115/1.2841305
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