Multidisciplinary Design Optimization of Film-Cooled Gas Turbine Blades

Shashishekara S. Talya, J. N. Rajadas, A. Chattopadhyay

Research output: Contribution to journalArticle

12 Citations (Scopus)

Abstract

Design optimization of a gas turbine blade geometry for effective film cooling to reduce the blade temperature has been done using a multiobjective optimization formulation. Three optimization formulations have been used. In the first, the average blade temperature is chosen as the objective function to be minimized. An upper bound constraint has been imposed on the maximum blade temperature. In the second, the maximum blade temperature is chosen as the objective function to be minimized with an upper bound constraint on the average blade temperature. In the third formulation, the blade average and maximum temperatures are chosen as objective functions. Shape optimization is performed using geometric parameters associated with film cooling and blade external shape. A quasi-three-dimensional Navier-Stokes solver for turbomachinery flows is used to solve for the flow field external to the blade with appropriate modifications to incorporate the effect of film cooling. The heat transfer analysis for temperature distribution within the blade is performed by solving the heat diffusion equation using the finite element method. The multiobjective Kreisselmeier-Steinhauser function approach has been used in conjunction with an approximate analysis technique for optimization. The results obtained using both formulations are compared with reference geometry. All three formulations yield significant reductions in blade temperature with the multiobjective formulation yielding largest reduction in blade temperature.

Original languageEnglish (US)
Pages (from-to)97-119
Number of pages23
JournalMathematical Problems in Engineering
Volume5
Issue number2
StatePublished - 1999

Fingerprint

Multidisciplinary Design Optimization
Gas Turbine
Turbine Blade
Blade
Turbomachine blades
Gas turbines
Film Cooling
Formulation
Temperature
Cooling
Bound Constraints
Objective function
Geometry
Design optimization
Turbomachinery
Shape optimization
Multiobjective optimization
Upper bound
Heat Diffusion
Optimization

Keywords

  • Film cooling
  • Heat transfer
  • Multidisciplinary
  • Optimization
  • Turbine blade

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Multidisciplinary Design Optimization of Film-Cooled Gas Turbine Blades. / Talya, Shashishekara S.; Rajadas, J. N.; Chattopadhyay, A.

In: Mathematical Problems in Engineering, Vol. 5, No. 2, 1999, p. 97-119.

Research output: Contribution to journalArticle

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