The Interactive Design Approach for Aerodynamic Shape Design Optimisation of the Aegis UAV

In this work, an interactive optimisation framework—a combination of a low fidelity flow solver, Athena Vortex Lattice (AVL), and an interactive Multi-Objective Particle Swarm Optimisation (MOPSO)—is proposed for aerodynamic shape design optimisation of any aerial vehicle platfor...

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Bibliographic Details
Main Authors: Yousef Azabi, Al Savvaris, Timoleon Kipouros
Format: Article
Language:English
Published: MDPI AG 2019-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/6/4/42