Aerodynamic Design Optimization of a Morphing Leading Edge and Trailing Edge Airfoil–Application on the UAS-S45

Aerodynamic Design Optimization of a Morphing Leading Edge and Trailing Edge Airfoil–Application on the UAS-S45

This work presents an aerodynamic optimization method for a Droop Nose Leading Edge (DNLE) and Morphing Trailing Edge (MTE) of a UAS-S45 root airfoil by using Bezier-PARSEC parameterization. The method is performed using a hybrid optimization technique based on a Particle Swarm Optimization (PSO) al...

Full description

Bibliographic Details
Main Authors: Musavir Bashir, Simon Longtin-Martel, Ruxandra Mihaela Botez, Tony Wong
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Applied Sciences
Subjects:
morphing airfoil optimization
parameterization
PSO
aerodynamic performance
Online Access:https://www.mdpi.com/2076-3417/11/4/1664

Internet

https://www.mdpi.com/2076-3417/11/4/1664

Similar Items