Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio

[+] Author and Article Information
A. K. Sinha, D. G. Bogard, M. E. Crawford

Mechanical Engineering Department, University of Texas at Austin, Austin, TX 78712

J. Turbomach 113(3), 442-449 (Jul 01, 1991) (8 pages) doi:10.1115/1.2927894 History: Received January 11, 1990; Online June 09, 2008


Film-cooling effectiveness was studied using a row of inclined holes that injected cryogenically cooled air across a flat, adiabatic test plate. The density ratio of the coolant to mainstream varied from 1.2 to 2.0. Surface temperatures were measured using a unique surface thermocouple arrangement free of conduction errors. Temperatures were obtained along the jet centerline and across a number of lateral locations. By independently varying density ratio and blowing rate, scaling of adiabatic effectiveness with mass flux ratio, velocity ratio, and momentum ratio was determined. Depending on the momentum flux ratio, the jet either remains attached to the surface, detaches and then reattaches, or is fully detached. For attached jets, the centerline effectiveness scaled with the mass flux ratio. However, for detached-reattached jets, a consistent scaling was not found although the general distribution of the centerline effectiveness scaled with momentum flux ratio. Laterally averaged effectiveness was found to be dependent on density ratio and momentum flux ratio. Decreases in density ratio and increases in momentum flux ratio were found to reduce the spreading of the film cooling jet significantly and thereby reduce laterally averaged effectiveness.

Copyright © 1991 by The American Society of Mechanical Engineers
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