Aircraft Propeller Design through Constrained Aero-Structural Particle Swarm Optimization

Aircraft Propeller Design through Constrained Aero-Structural Particle Swarm Optimization

An aero-structural algorithm to reduce the energy consumption of a propeller-driven aircraft is developed through a propeller design method coupled with a Particle Swarm Optimization (PSO). A wide range of propeller parameters is considered in the optimization, including the geometry of the airfoil...

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Bibliographic Details
Main Authors: José D. Hoyos, Jesús H. Jiménez, Camilo Echavarría, Juan P. Alvarado, Germán Urrea
Format: Article
Language:English
Published: MDPI AG 2022-03-01
Series:Aerospace
Subjects:
propeller
multidisciplinary optimization
particle swarm optimization
aero-structural optimization
Computational Fluids Dynamics
XFOIL
Online Access:https://www.mdpi.com/2226-4310/9/3/153

Internet

https://www.mdpi.com/2226-4310/9/3/153

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