@inproceedings{87c7ab2ca57f4fa4959aaa9b5044a266,
title = "Panel flutter and aerodynamic noise attenuation through aero-servo-viscoelastic controls",
abstract = "Dynamic responses of linear viscoelastic flat panels (plates) under the influence of aerodynamic noise are formulated and examined. Three modes of potential failures are considered, namely panel flutter, creep buckling and material failure such as composite fiber delamination. Differential, integral or proportional servo-controlers are added in order to stabilize the system and extend its lifetime. Parametric studies of servo-controllers led to no general conclusion because of the highly complicated phase relations. However, the simulations indicate that an increase in servo control parameters does not necessarily lead to an increase in flutter velocity.",
keywords = "Aero-servo-viscoelasticity, Failure probability, Panel flutter, Servo controls, Structural control, Survival times, Viscoelasticity",
author = "Merrett, {Craig G.} and Hilton, {Harry H.}",
year = "2009",
doi = "10.2514/6.2009-2512",
language = "English (US)",
isbn = "9781563479731",
series = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "17th AIAA/ASME/AHS Adaptive Structures Conf., 11th AIAA Non-Deterministic Approaches Conf., 10th AIAA Gossamer Spacecraft Forum, 5th AIAA Multidisciplinary Design Optimization Specialist Conf., MDO",
}