Nowadays, there is a growing need for flying drones with diverse capabilities for both civilian
and military applications. There is also a significant interest in the development of novel …

An advanced potential flow method is used to study the aerodynamic interactions between
small rotors of quadrotor configurations and the impact on the overall flight performance. The …

Fluid–structure interaction (FSI) analysis is often highly computationally expensive, making it
infeasible to conduct iterative aeroelastic design studies or rigorous optimizations. This work …

One of the important steps in the sizing process of fixed and flapping wing micro air vehicles
(MAVs) is weight estimation of the electrical and structural components. In order to enhance …

Flapping rotary wing (FRW) is a promising wing layout applicable to micro air vehicles
design due to its capability in high lift production. Previous aerodynamic investigations of …

Aeroelastic problems are commonly evaluated using tools such as fluid-structure interaction
(FSI) analysis. However, performing design studies or optimizations with FSI analysis is …

Investigated and revealed are new insights into the individual, decoupled effects of induced
camber and spanwise bending on the lift, drag, and endurance for an optimum flexibility …

Aerodynamic research is primarily divided into two parts; fly higher, fly faster and fly low, fly
slow. This research is focused towards the later part of aerodynamic advancements, which …

In this study, flow field analysis was performed to determine the aerodynamic coefficients for
the SC36210 and NACA0018 airfoil profiles in supersonic compressible flow at 2 Mach …

Fluid-structure interaction (FSI) analysis is a common tool used to analyze aeroelastic
problems. The traditional FSI scheme couples independent structure and fluid solvers in …