28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-11.10.3
ROBUST AERODYNAMIC DESIGN OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA
D. S. Lee, L. F. Gonzalez*, J. Periaux**, E. Onate**
CIMNE, Spain & Deloitte Consulting LLC, Korea; *ARCAA, QUT, Australia; **CIMNE & UPC, Spain
Keywords: robust/uncertainty design, multi-objective genetic algorithms (moga), parallel computing, morphing wing
In this paper, one of morphing technologies: leading/trailing edge deformation technique on one of the natural laminar flow aerofoils (RAE5243)is considered to reduce transonic drag. The paper illustrates the potential morphing technique for flow control as a near future aeronautical technique to be used in a civil aviation.
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