Shape optimization of turbine blades with the integration of aerodynamics and heat transfer

J. N. Rajadas, A. Chattopadhyay, N. Pagaldipti, S. Zhang

Research output: Contribution to journalArticle

7 Citations (Scopus)

Abstract

A multidisciplinary optimization procedure, with the integration of aerodynamic and heat transfer criteria, has been developed for the design of gas turbine blades. Two different optimization formulations have been used. In the first formulation, the maximum temperature in the blade section is chosen as the objective function to be minimized. An upper bound constraint is imposed on the blade average temperature and a lower bound constraint is imposed on the blade tangential force coefficient. In the second formulation, the blade average and maximum temperatures are chosen as objective functions. In both formulations, bounds are imposed on the velocity gradients at several points along the surface of the airfoil to eliminate leading edge velocity spikes which deteriorate aerodynamic performance. Shape optimization is performed using the blade external and coolant path geometric parameters as design variables. Aerodynamic analysis is performed using a panel code. Heat transfer analysis is performed using the finite element method. A gradient based procedure in conjunction with an approximate analysis technique is used for optimization. The results obtained using both optimization techniques are compared with a reference geometry. Both techniques yield significant improvements with the multiobjective formulation resulting in slightly superior design.

Original languageEnglish (US)
Pages (from-to)21-42
Number of pages22
JournalMathematical Problems in Engineering
Volume4
Issue number1
StatePublished - 1998

Fingerprint

Turbine Blade
Shape Optimization
Shape optimization
Blade
Aerodynamics
Turbomachine blades
Heat Transfer
Turbines
Heat transfer
Formulation
Bound Constraints
Optimization
Objective function
Gradient
Airfoils
Gas Turbine
Coolants
Temperature
Gas turbines
Airfoil

Keywords

  • Aerodynamics
  • Heat transfer
  • Multidisciplinary
  • Optimization
  • Turbine blades

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Shape optimization of turbine blades with the integration of aerodynamics and heat transfer. / Rajadas, J. N.; Chattopadhyay, A.; Pagaldipti, N.; Zhang, S.

In: Mathematical Problems in Engineering, Vol. 4, No. 1, 1998, p. 21-42.

Research output: Contribution to journalArticle

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