Antony Jameson pioneered CFD-based aerodynamic design optimization in the late 1980s.
In addition to develo** the fundamental theory, Jameson implemented that theory in …

Flutter is a dynamic aeroelastic instability driven by the interaction of inertial, elastic, and
aerodynamic forces. It is an undesirable phenomenon in aircraft because it causes divergent …

Current economic constraints and environmental regulations call for design of more efficient
aircraft configurations. An observed trend in aircraft design to reduce the lift induced drag …

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 …

In this paper, the advantages, state-of-the-art, and current challenges in the field of adaptive
composite marine propulsors and turbines are reviewed. Adaptive composites are used in …

The paper develops a reduction scheme based on the identification of continuous time
recursive neural networks from input–output data obtained through high fidelity simulations …

Physical interactions between a fluid and structure, potentially manifested as self-sustained
or divergent oscillations, can be sensitive to many parameters whose values are uncertain …

Ensuring adequate flutter margins is a critical step in aircraft design. However, in the
presence of nonlinear effects, subcritical limit-cycle oscillations can arise even before flutter …

This paper provides a brief overview of the state-of-the-art for aeroelastic tailoring of
subsonic transport aircraft and offers additional resources on related research efforts …

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 …