Two-Way Coupled Aero-Structural Optimization of Stable Flying Wings
An aero-structural algorithm to optimize a flying wing in cruise conditions for preliminary design is developed using two-way interaction between the structure and aerodynamics. A particle swarm routine is employed to solve the multi-objective optimization, aiming to reduce the weight of the structu...
Main Authors: | José D. Hoyos, Camilo Echavarría, Juan P. Alvarado, Gustavo Suárez, Juliana A. Niño, Jorge I. García |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-04-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/4/346 |
Similar Items
-
Aircraft Propeller Design through Constrained Aero-Structural Particle Swarm Optimization
by: José D. Hoyos, et al.
Published: (2022-03-01) -
Multidisciplinary Analysis and Optimization Method for Conceptually Designing of Electric Flying-Wing Unmanned Aerial Vehicles
by: Oscar Ulises Espinosa Barcenas, et al.
Published: (2022-10-01) -
Design Investigation of Potential Long-Range Hydrogen Combustion Blended Wing Body Aircraft with Future Technologies
by: Stanislav Karpuk, et al.
Published: (2023-06-01) -
Parametric Investigation of Canards on a Flying Wing UAV Using the Taguchi Method
by: Stavros Kapsalis, et al.
Published: (2023-03-01) -
Multi-objective aerodynamic optimization of flying-wing configuration based on adjoint method
Published: (2021-08-01)