Multdisciplinary design optimization of film-cooled gas turbine blades

Shashishekara S. Talya, John Rajadas, Aditi Chattopadhyay

Research output: Chapter in Book/Report/Conference proceedingChapter

7 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.

Original languageEnglish (US)
Title of host publicationAmerican Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD
Pages59-64
Number of pages6
Volume357
Edition4
StatePublished - 1998

Fingerprint

Turbomachine blades
Gas turbines
Temperature
Cooling
Geometry
Turbomachinery
Shape optimization
Multiobjective optimization
Design optimization
Flow fields
Temperature distribution
Heat transfer
Finite element method

ASJC Scopus subject areas

  • Fluid Flow and Transfer Processes
  • Mechanical Engineering

Cite this

Talya, S. S., Rajadas, J., & Chattopadhyay, A. (1998). Multdisciplinary design optimization of film-cooled gas turbine blades. In American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD (4 ed., Vol. 357, pp. 59-64)

Multdisciplinary design optimization of film-cooled gas turbine blades. / Talya, Shashishekara S.; Rajadas, John; Chattopadhyay, Aditi.

American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD. Vol. 357 4. ed. 1998. p. 59-64.

Research output: Chapter in Book/Report/Conference proceedingChapter

Talya, SS, Rajadas, J & Chattopadhyay, A 1998, Multdisciplinary design optimization of film-cooled gas turbine blades. in American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD. 4 edn, vol. 357, pp. 59-64.
Talya SS, Rajadas J, Chattopadhyay A. Multdisciplinary design optimization of film-cooled gas turbine blades. In American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD. 4 ed. Vol. 357. 1998. p. 59-64
Talya, Shashishekara S. ; Rajadas, John ; Chattopadhyay, Aditi. / Multdisciplinary design optimization of film-cooled gas turbine blades. American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD. Vol. 357 4. ed. 1998. pp. 59-64
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