Titlebook: IUTAM Symposium on Smart Structures and Structronic Systems; Proceedings of the I U. Gabbert,H. S. Tzou Conference proceedings 2001 Springe

垫子

978-94-010-3836-2Springer Science+Business Media Dordrecht 2001

ONYM

吹牛大王

0925-0042 Overview: 978-94-010-3836-2978-94-010-0724-5Series ISSN 0925-0042 Series E-ISSN 2214-7764

评论者

Simultaneous Active Damping and Health Monitoring of Aircraft Panels,h monitoring and active damping of panels characteristic of aircraft components. Here smart structures refers to the integrated use of piezoelectric actuators and fiber optic sensors as the measurement transducers and control actuators required to actively damp a panel and to provide health monitori

加强防卫

Decentralized Vibration Control and Coupled Aeroservoelastic Simulation of Helicopter Rotor Blades irfoil shape is adaptive, the aerodynamic loads can be affected to reduce vibration and moreover, the airfoil shape can be adjusted to the periodically changing flow conditions to increase aerodynamic efficiency. Adaptation of the airfoil shape may be achieved by discrete trailing edge flaps or cont

灾难

Design of Reduced-Order Controllers on a Representative Aircraft Fuselage, passive control becomes massive for control of low frequency disturbances. Model-based active controllers are difficult to apply to complex structures, because the model needs to be of roughly the same order as the system that it describes in order to achieve robust performance. Modeling errors due

fibula

暴行

煞费苦心

注射器

Modelling and Optimisation of Passive Damping for Bonded Repair to Acoustic Fatigue Cracking,ed repairs have been implemented quite successfully in a variety of aircraft applications for the past twenty years, a recent application to repair acoustic-fatigue cracking on the engine nacelle of the F/A-18 has proved ineffective [.], contrary to expectations from current design practice for such