Aerodynamic shape optimization of rotary wing aircraft components using an advanced multiobjective evolutionary approach - Archive ouverte HAL
Communication Dans Un Congrès Année : 2013

Aerodynamic shape optimization of rotary wing aircraft components using an advanced multiobjective evolutionary approach

Claudio Comis da Ronco
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Résumé

In the framework of my Ph.D. course, I developed a novel Multi-objective Evolutionary Algorithm (MOEA), namely the GeDEA-II, which features a Simplex-based crossover operator. The comparison among GeDEA-II and three modern elitist methods, on state-of-the-art multi-objective problems, clearly indicates that the performance of GeDEA-II is superior. Finally, a test case is presented, regarding the aerodynamic shape optimization of the AgustaWestland 101 helicopter left air intake.
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Dates et versions

hal-00855849 , version 1 (30-08-2013)

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  • HAL Id : hal-00855849 , version 1

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Claudio Comis da Ronco. Aerodynamic shape optimization of rotary wing aircraft components using an advanced multiobjective evolutionary approach. 2nd ECCOMAS Young Investigators Conference (YIC 2013), Sep 2013, Bordeaux, France. ⟨hal-00855849⟩

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