Application of Multi Objective Constrained Optimization in Aerodynamic High Lift Desing
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چکیده
This lecture deals with the application of numerical optimization for aerodynamic design of high-lift systems, which is a multi-objective constraint design problem. The applied mathematical fundamentals of numerical optimization are briefly outlined. A description of the design targets and constraints for high-lift wings is given, followed by a detailed analysis of the properties of the flow calculation for the use within optimization and the suitability of optimization algorithms for this type of design problem. Another focus is set on the practical issues resulting from a long time experience in applying numerical optimization to aerodynamic design. of high-lift systems for transport aircraft.
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تاریخ انتشار 2005