Studies of preview gust load alleviation H 2 and H∞ controllers via synthesis, simulation,
wind tunnel tests, and test/simulation correlation are presented in this paper. University of …

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 …

This paper introduces a new metric to constrain postflutter responses of aeroelastic systems
in design optimization. The new metric aggregates the recovery rate to equilibrium for a …

Reduced-order models (ROM) have captured the interest and effort of many investigators
over the years. As is well known the cost of computation can easily outpace the available …

This paper aims to gain new insight into the physical mechanism of laminar separation flutter
(LSF) from the perspective of energy transfer and dynamic mode decomposition (DMD) …

The computational fluid dynamic/computational structural dynamic (CFD/CSD) coupling
method plays an important role in static aeroelastic problems accounting for structural …

This paper introduces a method for estimating flutter bifurcation diagrams of systems
described by time-domain state-space models. The method estimates the bifurcation …

The Third Aeroelastic Prediction Workshop Large Deflection Working Group (AePW3-
LDWG) revolves around the Pazy wing, a geometrically nonlinear benchmark model for …