Session: 12-01: Additive Manufacturing in Film Cooling

Paper Number: 153014

The Influence of In-Hole Roughness on Leading Edge Overall Effectiveness 

The impact of surface roughness on gas turbine heat transfer has been of interest for many years, but relatively little attention has been paid to the effects on in-hole roughness. Even then, most efforts have been aimed at characterizing the influence of internal roughness on the heat transfer coefficient or the resulting impact on adiabatic effectiveness. That important previous work has documented roughness’s deleterious effects on the adiabatic effectiveness, but these are coupled with improved internal heat transfer coefficients. Characterization of these competing effects of internal roughness on the overall effectiveness has received little attention.

In the present work, overall effectiveness experiments were conducted using a model of a leading edge showerhead. The approximately 10x scale model was made of hydrodynamically smooth conducting material to provide a Biot number representative of typical turbine components and allow determination of the overall effectiveness distribution for a baseline case of a smooth surface finish. Three additional combinations of rough surfaces were used to examine their influence on overall effectiveness—one with the exterior surface roughened, one with the interiors of the cooling holes roughened and finally, one with both the holes and the external surface roughened. Surface roughness was provided by adhering filtered sand to the surfaces of interest, providing a root mean square roughness to hole diameter ratio of R_q/d = 0.025 and arithmetic mean roughness to hold diameter ratio of R_a/d = 0.020. This unique combination of roughness experiments allowed for segregation of the effects of interior hole roughness from the effects of the rough external surface. The interior hole roughness has competing effects on the overall effectiveness through a reduction in external film cooling performance, but at the same time, improved internal cooling. These competing effects were clear with overall effectiveness improvements occurring in regions where internal cooling dominates and degradations occurring where film cooling plays a larger role in overall effectiveness distributions.

Presenting Author: Bailey Hopkins Air Force Institute of Technology

Presenting Author Biography: Bailey Hopkins is a graduate of the Air Force Institute of Technology and works as a developmental engineer at the Air Force Research Laboratory.

Authors:

Bailey Hopkins Air Force Institute of Technology
James L. Rutledge Air Force Institute of Technology