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Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating

Journal Article · · Journal of Turbomachinery
DOI:https://doi.org/10.1115/1.4053840· OSTI ID:1982933
 [1];  [1];  [1];  [2];  [1]
  1. Walker Department of Mechanical Engineering, The University of Texas at Austin, Austin, TX 78712
  2. Oden Institute for Computational Engineering and Sciences, The University of Texas at Austin, Austin, TX 78712

Abstract Few studies in the open literature have studied the effect of thermal barrier coatings (TBC) when used in combination with shaped hole film cooling and enhanced internal cooling techniques. The current study presents Reynolds-averaged Navier–Stokes (RANS) conjugate heat transfer simulations that identify trends in cooling design performance as well as experimental measurements of overall effectiveness using a flat-plate matched-Biot number model with a simulated TBC layer of 0.42D thickness, where D is the film cooling hole diameter. Coolant is fed to the film cooling holes in a co-flow configuration, and the results of both the smooth and rib-turbulated channels are compared. At a constant coolant flow rate, enhanced internal cooling was found to provide a 44% increase in spatially-averaged overall effectiveness, $$\bar{\bar{\phi}}$$, without a TBC. The results show that the addition of a TBC can raise $$\bar{\bar{\phi}}$$ on a film-cooled component surface by 47%. The optimum velocity ratio was found to decrease with the addition of enhanced cooling techniques and a TBC as the film provided minimal benefit at the expense of reduced internal cooling. While the computational results closely identified trends in overall system performance without a TBC, the model over-predicted effectiveness on the metal–TBC interface. The results of this study will inform turbine component design as material science advances increase the reliability of the TBC.

Research Organization:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV, Albany, OR (United States)
Sponsoring Organization:
USDOE
OSTI ID:
1982933
Journal Information:
Journal of Turbomachinery, Vol. 144, Issue 9; ISSN 0889-504X
Publisher:
ASME
Country of Publication:
United States
Language:
English

References (18)

Discharge Coefficient Measurements of Film-Cooling Holes With Expanded Exits conference June 1997
Evolution of Turbine Cooling
  • Bunker, Ronald S.
  • ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards https://doi.org/10.1115/GT2017-63205
conference August 2017
Effects of TBC Thickness on an Internally and Film Cooled Model Turbine Vane conference June 2014
Describing the uncertainties in experimental results journal January 1988
Rib Turbulator Effects on Crossflow-Fed Shaped Film Cooling Holes journal January 2019
The Effects of Manufacturing Tolerances on Gas Turbine Cooling journal July 2009
The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications journal January 1994
Augmented Heat Transfer in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs journal August 1991
Overall and Adiabatic Effectiveness Values on a Scaled Up, Simulated Gas Turbine Vane journal June 2013
Experimental Simulation of a Film Cooled Turbine Blade Leading Edge Including Thermal Barrier Coating Effects journal September 2010
Evaluating the Usefulness of RANS in Film Cooling conference June 2019
Gas Turbine Film Cooling journal March 2006
Film Cooling With a Thermal Barrier Coating: Round Holes, Craters, and Trenches journal September 2013
Roughness Effects on Flow and Heat Transfer for Additively Manufactured Channels journal January 2016
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness—Part I: Axial Shaped Holes journal October 2017
Effect of Internal Coolant Crossflow Orientation on the Discharge Coefficient of Shaped Film-Cooling Holes journal February 1999
Experimental Measurements and Computational Predictions for an Internally Cooled Simulated Turbine Vane journal August 2012
Parametric Optimization of Film Cooling Hole Geometry conference June 2021