Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation

نویسندگان

چکیده

Advanced optimisation of the aerofoil wing a general aircraft is main subject this paper. Meta-heuristic techniques, especially swarm algorithms, were used. Subsequently, new variant denoted as particle (aPSO) was developed from original (PSO). A parametric model based on B-spline used to optimise initial aerofoil. The simulation software Xfoil calculating basic aerodynamic features (lift, drag, moment).

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ژورنال

عنوان ژورنال: Mendel ...

سال: 2022

ISSN: ['1803-3814', '1803-3822', '2571-3701']

DOI: https://doi.org/10.13164/mendel.2022.1.063