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 …

This paper is written as a contribution to the celebration of 50 years of Progress in
Aerospace Sciences and of the centenary of the birth of its founder, Dietrich Küchemann. It …

The objective of the present paper is improving the effectiveness of a winglet control surface
at deflections greater than≈ 5° through passive vortex generators (VG) placed on the …

Abstract Operational Modal Analysis (OMA) is a promising candidate for flutter testing and
Structural Health Monitoring (SHM) of aircraft wings that are passively excited by wind loads …

Static aerodynamic force measurement is generally of interest in both low-and high-speed
ground test facilities, but dynamic force measurement is typically associated with higher …

A numerical tool for the computation of aircraft control surface aerodynamics with flexibility
effects is presented. The solution is based on coupled Computational Fluid Dynamics (CFD) …

This paper summarizes the plans for the first Aeroelastic Prediction Workshop. The
workshop is designed to assess the state of the art of computational methods for predicting …

This paper summarizes data and findings from the first Aeroelastic Prediction Workshop
(AePW) held in April, 2012. The workshop has been designed as a series of technical …

Numerical aeroelastic investigations are conducted for the Model53 delta wing with a
deployed slat and two trailing-edge control surfaces at transonic speed and high dynamic …

This paper presents numerical results in comparison with experimental data of nominally
static aeroelastic polars of the second ASDMAD (Aero-Structural Dynamics Methods for …