04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM
F.I. Carvalhoš, R.G. Silvaš; šITA, Brazil
This paper will evaluate a mathematical model of 3 degrees of freedom, with different coupling factors between flaps (leading and trailing edges) for increased flutter velocity, known as the LAMBIE model1. The aeroelastic study will present the numerical methodology for simulations of the model of 3ndegrees of freedom presenting coupling factors between the flaps