Aerodynamic optimization of transonic cascade using global aerodynamic optimization method;

Multi-parameter aerodynamic optimization method for a 3D turbine stator blades;

Aerodynamic Optimization Design Method of Turbine Blade and Exhaust System;

Applying automatic aerodynamic optimization method of 3D cascade,the first stage nozzle of E~3 turbine was optimized for the maximization of the total pressure coefficient by constraining the mass flow rate and total pressure ratio.

Application of genetic algorithm to multi-stage compressor aerodynamic optimization design;

Research of aerodynamic optimization methodbased on dynamic boundary control;

Based on the reliable region methodology, combined with the CFD simulations from both of the N-S and Euler equations,an aerodynamic optimization scheme with gradient-based approximation management framework(AMF) is proposed, where the variable-fidelity models collecting full advantages of the low-fidelity models are organized and managed.

The application of Pareto GAs to aerodynamic configuration design;

Due to the massive computation load and time as well as an excessively huge variable-sample database space specific to the three-dimensional aerodynamic optimization design of a multi-stage turbine,a long design cycle often results,which is difficult to cope with effectively in practice.

The paper expresses aerodynamic optimization design of lower Reynold number high-lift airfoils using genetic algorithm,wind-tunnel experimental of design airfoil tests correctness of design.

The paper presented here demonstrates the application of genetic algorithm on aerodynamic optimization design of lower Reynold number high-lift airfoils and optimized airfoil have a considerable improvement on aerodynamic performance,show the feasibility of genetic algorithm applied on aerodynamic optimization design.