In this work, a novel data-based stochastic “global” identification framework is introduced for
aerospace structures operating under varying flight states and uncertainty. In this context …

This article presents the application of aeroelastic tailoring in the design of wings for a flying
demonstrator, as well as the validation of the design methodology with flight test results. The …

A novel Data-driven State Awareness (DSA) framework is introduced for the next generation
of intelligent “fly-by-feel” aerospace vehicles. The proposed framework is based on two …

In this work, a data-driven approach for identifying the flight state of a self-sensing wing
structure with an embedded multi-functional sensing network is proposed. The flight state is …

Application of the aeroelastic analysis and design framework developed at Delft University
of Technology to a design of two aeroelastically tailored composite wings for a flying …

Nonlinear dynamic aeroelasticity of composite wings in compressible flows is investigated.
To provide a reasonable model for the problem, the composite wing is modeled as a thin …

Aeroelastic tailoring offers an effective way to exploit the anisotropic properties of the
composite materials used in lightweight aerospace structures. This paper presents a design …

This paper presents the application of aeroelastic tailoring in the wing design of a flying
demonstrator. The work is part of the Flutter Free Flight Envelope eXpansion (FLEXOP) …

In this work, a novel Data-driven State Awareness (DSA) framework is introduced for the
next generation of intelligent “fly-by-feel” aerospace vehicles. The proposed framework is …

Viscoelastic composite materials use has increased in aircraft structures. These materials
have time-dependent behaviours that have not been fully investigated for certain aeroelastic …