SECOND LAW ANALYSIS OF FILM COOLING

Second Law Analysis of Film Cooling
● Use of second law analysis to quantify aerodynamic and thermal energy losses.
● Consideration of a variety of film cooling configurations, and cambered vanes with and without film cooling.
● Quantification of temperature and pressure variations, as well as aerodynamic gains, using second law analysis.
● Also considered are interrelationships of entropy production and turbulence kinetic energy associated with simple angle and compound angle full coverage film cooling.

REFERENCES:
Second Law Analysis of Aerodynamic Losses: Results for a Cambered Vane With and Without Film Cooling (P. M. Ligrani, and J. S. Jin), ASME Transactions-Journal of Turbomachinery, Vol. 135, No. 4, pp. 041013-1 to 041013-14, July 2013.

Numerical Second Law Analysis Around a Turbine Guide Vane Using a Two-Equation Turbulence Model and Comparison With Experiments (S. Winkler, E. Kerber, T. Hitz, B. Weigand, and P. M. Ligrani), International Journal of Thermal Sciences, Vol. 116, pp. 91-102, June 2017.

Second Law Analysis of Aerodynamic Gains Associated With Simple Angle and Compound Angle Full Coverage Film Cooling (S. R. Vanga, and P. M. Ligrani), International Journal of Thermophysics, Vol. 42, Article No. 154, pp. 1- 27, August 2021.

Second Law Analysis of Aerodynamic Characteristics With Flow Temperature Variations of Simple Angle and Compound Angle Full Coverage Film Cooling (S. R. Vanga, and P. M. Ligrani), International Journal of Thermal Sciences, Vol. 176, Paper No. 107511, pp. 1-13, June 2022.

Interrelationships of Entropy Production and Turbulence Kinetic Energy Associated With Simple Angle and Compound Angle Full Coverage Film Cooling (P. M. Ligrani, H. Kwon, and H. Park), International Journal of Thermal Sciences, Volume 197, Paper No. 108824, pp. 1-19, March 2024.

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