Film cooling flow for reduction in heat flux to a gas turbine engine hot gas path component is generally assumed to be steady. However, unsteady film cooling may occur due to naturally occurring flow unsteadiness or may be induced intentionally. Analysis of pulsed or otherwise unsteady film coolant flow necessitates a reformulation of the existing steady-state technique for net heat flux reduction (NHFR). We show that addition of a cross-coupled term to the traditional steady form of the NHFR equation with time averaged quantities accounts for the unsteady effects. In the experimental technique to determine the time averaged NHFR, we present a new parameter to capture the combined influence of the average adiabatic effectiveness and the coupling between and . Measurement of is shown to be straightforward but requiring careful considerations beyond those required to measure with steady film cooling.
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e-mail: james.rutledge@us.af.mil
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December 2010
Research Papers
Time Averaged Net Heat Flux Reduction for Unsteady Film Cooling
James L. Rutledge,
James L. Rutledge
Air Force Institute of Technology,
e-mail: james.rutledge@us.af.mil
Wright-Patterson Air Force Base
, OH 45433
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Paul I. King,
Paul I. King
Air Force Institute of Technology,
Wright-Patterson Air Force Base
, OH 45433
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Richard Rivir
Richard Rivir
Air Force Research Laboratory,
Wright-Patterson Air Force Base
, OH 45433
Search for other works by this author on:
James L. Rutledge
Air Force Institute of Technology,
Wright-Patterson Air Force Base
, OH 45433e-mail: james.rutledge@us.af.mil
Paul I. King
Air Force Institute of Technology,
Wright-Patterson Air Force Base
, OH 45433
Richard Rivir
Air Force Research Laboratory,
Wright-Patterson Air Force Base
, OH 45433J. Eng. Gas Turbines Power. Dec 2010, 132(12): 121901 (6 pages)
Published Online: August 24, 2010
Article history
Received:
February 1, 2010
Revised:
April 24, 2010
Online:
August 24, 2010
Published:
August 24, 2010
Citation
Rutledge, J. L., King, P. I., and Rivir, R. (August 24, 2010). "Time Averaged Net Heat Flux Reduction for Unsteady Film Cooling." ASME. J. Eng. Gas Turbines Power. December 2010; 132(12): 121901. https://doi.org/10.1115/1.4001810
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