[HTML][HTML] A review of bird-like flap** wing with high aspect ratio

XIE Changchuan, GAO Nongyue, M Yang… - Chinese Journal of …, 2023 - Elsevier
Bird-like flap**-wing vehicles with a high aspect ratio have the potential to fulfill missions
given to micro air vehicles, such as high-altitude reconnaissance, surveillance, rescue, and …

High-performance morphing wing for large-scale bio-inspired unmanned aerial vehicles

E Savastano, V Perez-Sanchez… - IEEE Robotics and …, 2022 - ieeexplore.ieee.org
This letter proposes a novel bio-inspired wing design to improve some characteristics of
Flap** Wing Unmanned Vehicles (FWUV) related to their potential applications such as …

Code-to-code benchmark for simulation tools based on the unsteady vortex-lattice method

ML Verstraete, LR Ceballos, C Hente… - Journal of Aerospace …, 2023 - arc.aiaa.org
Reliable aerodynamic and aeroelastic simulations of advanced aeronautical/mechanical
systems require us to predict flow-induced forces as accurately as possible. Nowadays …

Kutta–Joukowski theorem for unsteady linear aerodynamics

M Gennaretti, R Giansante - AIAA Journal, 2022 - arc.aiaa.org
This paper presents the extension of the Kutta–Joukowski theorem to unsteady linear
aerodynamics. Starting from the formulation developed by Theodorsen for the solution of the …

Unsteady aerodynamic analysis and effectiveness of bio-inspired flap** wings in V-formation flight

E Billingsley, M Ghommem… - Proceedings of the …, 2023 - journals.sagepub.com
Several bird species have been observed to fly in V-formation, an arrangement which
exploits aerodynamic features to allow the group to conserve energy when migrating over …

Reduced coupled flap** wing-fluid computational model with unsteady vortex wake

Z Terze, V Pandža, M Andrić, D Zlatar - Nonlinear dynamics, 2022 - Springer
Insect flight research is propelled by their unmatched flight capabilities. However, complex
underlying aerodynamic phenomena make computational modeling of insect-type flap** …

A general modal frequency-domain vortex lattice method for aeroelastic analyses

M Parenteau, E Laurendeau - Journal of Fluids and Structures, 2020 - Elsevier
The generalized aerodynamic force (GAF) matrix is derived for the Unsteady Vortex Lattice
Method (UVLM) without the assumption of out-of-plane dynamics. As a result, the approach …

[HTML][HTML] A Comparison of Modern Metaheuristics for Multi-Objective Optimization of Transonic Aeroelasticity in a Tow-Steered Composite Wing

K Phuekpan, R Khammee, N Panagant, S Bureerat… - Aerospace, 2025 - mdpi.com
This study proposes a design procedure for the multi-objective aeroelastic optimization of a
tow-steered composite wing structure that operates at transonic speed. The aerodynamic …

Modelling and Handling Quality Assessment of the Flying-V Aircraft

S van Overeem, X Wang, EJ Van Kampen - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1429. vid Considerable growth in
the number of passengers and cargo transported by air is predicted. Besides that, aircraft …

Validation and Optimization of Ptera Software: An Open-Source Unsteady Flow Simulator for Flap** Wings

C Urban, RK Agarwal - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1967. vid Scientists have long
used the unsteady vortex lattice method (UVLM) to simulate flap**-wing flight. However …