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Main Authors: Sheikh, Haris Moazam, Lee, Sangjoon, Wang, Jinge, Marcus, Philip S.
Format: Preprint
Published: 2022
Subjects:
Online Access:https://arxiv.org/abs/2207.11448
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author Sheikh, Haris Moazam
Lee, Sangjoon
Wang, Jinge
Marcus, Philip S.
author_facet Sheikh, Haris Moazam
Lee, Sangjoon
Wang, Jinge
Marcus, Philip S.
contents We present Design-by-Morphing (DbM), a novel design methodology applicable to creating a search space for topology optimization of 2D airfoils. Most design techniques impose geometric constraints and sometimes designers' bias on the design space itself, thus restricting the novelty of the designs created, and only allowing for small local changes. We show that DbM methodology does not impose any such restrictions on the design space and allows for extrapolation from the search space, thus granting truly radical and large search space with a few design parameters. In comparison to other shape design methodologies, we apply DbM to create a search space for 2D airfoils. We optimize this airfoil shape design space for maximizing the lift-over-drag ratio, $CLD_{max}$, and stall angle tolerance, $Δα$. Using a bi-objective genetic algorithm to optimize the DbM space, it is found that we create a Pareto-front of radical airfoils exhibiting remarkable properties for both objectives.
format Preprint
id arxiv_https___arxiv_org_abs_2207_11448
institution arXiv
publishDate 2022
record_format arxiv
spellingShingle Airfoil Optimization using Design-by-Morphing
Sheikh, Haris Moazam
Lee, Sangjoon
Wang, Jinge
Marcus, Philip S.
Geometric Topology
Computational Engineering, Finance, and Science
Optimization and Control
We present Design-by-Morphing (DbM), a novel design methodology applicable to creating a search space for topology optimization of 2D airfoils. Most design techniques impose geometric constraints and sometimes designers' bias on the design space itself, thus restricting the novelty of the designs created, and only allowing for small local changes. We show that DbM methodology does not impose any such restrictions on the design space and allows for extrapolation from the search space, thus granting truly radical and large search space with a few design parameters. In comparison to other shape design methodologies, we apply DbM to create a search space for 2D airfoils. We optimize this airfoil shape design space for maximizing the lift-over-drag ratio, $CLD_{max}$, and stall angle tolerance, $Δα$. Using a bi-objective genetic algorithm to optimize the DbM space, it is found that we create a Pareto-front of radical airfoils exhibiting remarkable properties for both objectives.
title Airfoil Optimization using Design-by-Morphing
topic Geometric Topology
Computational Engineering, Finance, and Science
Optimization and Control
url https://arxiv.org/abs/2207.11448