Optimization of Aerodynamic Design of a Winged UAV Through Genetic Algorithms and Large Eddy Simulation
This paper focuses on the optimization of a winged UAV airframe utilizing a preliminary configuration and the combination of the Taguchi experimental design method and the evolutionary genetic optimization algorithm, along with computational fluid dynamics. Simulations were carried out based on the...
Saved in:
| Main Authors: | Mohammad Javad Ebrahimi, Mahmoud Pasandidehfard, Ali Esmaeili, Mohammad Hossein Moghimi Esfandabadi |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2024-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/ijae/2698950 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A Study on the Aerodynamic Impact of Rotors on Fixed Wings During the Transition Phase in Compound-Wing UAVs
by: Longjin Ai, et al.
Published: (2024-11-01) -
Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints
by: Durmuş Sinan Körpe, et al.
Published: (2019-01-01) -
Analysis of aerodynamic characteristics of hypersonic folding-wing aircraft
by: WU Zaoping, et al.
Published: (2024-12-01) -
The Aerodynamic Behavioral Study of Tandem Fan Wing Configuration
by: Du Siliang, et al.
Published: (2018-01-01) -
Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration
by: Daisuke Sasaki, et al.
Published: (2011-01-01)