Aerothermal Optimization and Experimental Verification for Discrete Turbine Airfoil Film Cooling
Author:
Affiliation:
1. Department of Mechanical and Industrial Engineering, Concordia University, Montreal, Quebec H3G1M8, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35235
Reference21 articles.
1. Effects of hole geometry and density on three-dimensional film cooling
2. Film Cooling From Shaped Holes
3. Film-cooling holes with expanded exits: near-hole heat transfer coefficients
4. Film Cooling Effectiveness for an Advanced-Louver Cooling Scheme for Gas Turbines
5. Effects of Orientation Angles on Film Cooling Over a Flat Plate: Boundary Layer Temperature Distributions and Adiabatic Film Cooling Effectiveness
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