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 …

The design of the propulsion system for Unmanned Aerial Vehicles (UAVs) demands an
inclusive multidisciplinary approach from the earliest design phases, since every design …

This paper considers the aeroelastic optimization of a subsonic transport wing box under a
variety of static and dynamic aeroelastic constraints. Three types of design variables are …

This paper examines the use of a variable-camber continuous trailing-edge flap system for
aeroservoelastic optimization of a transport wing box, the Common Research Model. Along …

Mission adaptive variable camber wing in both chord-wise and span-wise directions that can
improve the aerodynamic performance during takeoff, landing and cruising flight, will be the …

The single shooting method is applied to the optimal control and combined structural and
control design (co-design) of very flexible beams. The objective is to assess feasibility …

Design, Construction, and Tests of an Aeroelastic Wind Tunnel Model of a Variable Camber
Continuous Trailing Edge Flap (VCCTEF) Page 1 Design, Construction, and Tests of an …

AEROSERVOELASTIC optimization can be posed as a coupled plant-controller optimization
problem [1], where structural sizing and planform shape design variables define the aircraft …

Two aeroelastic design approaches are applied to a supersonic lambda wing configuration
with the goal of improving the wing's aeroelastic performance. Aeroelastic tailoring and …

In this paper, simultaneous computation of control gains and optimal sizing of control surface
parameters is considered such that the flutter boundary is extended by controlling the …