Active flutter suppression, which is a part of the group of flight vehicle technologies known as
active controls, is an important contributor to the effective solution of aeroelastic instability …

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 …

This is an introduction and overview of the work that has been done in nonlinear
aeroelasticity prior to the last decade. Many of the issues discussed here are still under …

Over the last fifty years, the ability to carry out analysis as a precursor to decision making in
engineering design has increased dramatically. In particular, the advent of modern …

The unsteady vortex-lattice method provides a medium-fidelity tool for the prediction of non-
stationary aerodynamic loads in low-speed, but high-Reynolds-number, attached flow …

The paper presents a theory for flight-dynamic analysis of highly flexible flying-wing
configurations. The analysis takes into account large aircraft motion coupled with …

ON 17 DECEMBER 1903, the Wright brothers set about the task of launching an airplane
into the sky. Their multiple successes that day have been hailed as the start of heavier-than …

THE studies in this paper are part of the development of an analysis framework for
performance prediction and flightcontrol-system (FCS) design of ultra-long-endurance solar …

Aeroelasticity is still dynamic, challenging, and a key part of cutting-edge airplane
technology. Emerging trends, as well as challenges and needs in the eld of airplane …

A mid-fidelity aerodynamic solver based on the vortex particle method for wake modeling,
DUST, is coupled through the partitioned multi-physics coupling library preCICE to a …