The traditional method for obtaining aerodynamic parameters of airfoils by solving Navier–
Stokes equations is a time-consuming computing task. In this article, a novel data-driven …

The paper presents the design, analyses, and testing of the Pazy wing, a very flexible wing
model that was designed to study aeroelastic phenomena associated with geometrically …

The paper presents the flutter and limit-cycle oscillation (LCO) tests of the Pazy wing, a very
flexible wing model designed to study aeroelastic phenomena associated with nonlinear …

This paper investigates the ability of low-order structural and aerodynamic models to predict
geometrically nonlinear aeroelastic behaviors associated with large wing deflections. The …

This paper investigates geometrically nonlinear effects due to nonlinear kinematics and
follower aerodynamics in the aeroelastic dynamics of a very flexible wing. The test case is …

Novel aircraft designs employing wings with high aspect ratio, such as the strut-braced wing
(SBW), are one way to reduce their environmental impact. However, the flexibility of longer …

In this paper, collaborative aeroelastic analyses of the\textit {Pazy Wing} are presented,
which support the activities of the Large Deflection Working Group, a sub-group of the 3rd …

The Pazy wing aeroelastic benchmark is a highly flexible wind tunnel model investigated in
the Large Deflection Working Group as part of the Third Aeroelastic Prediction Workshop …

Lightweight high-aspect-ratio wings make aircraft more energy efficient thanks to their lower
induced drag. Because such wings exhibit large deflections, design optimization based on …

This paper presents a nonlinear framework for the static and flutter analysis of highly flexible
wings accounting for large deformations, using a linear modal database. A nonlinear static …