垫子
发表于 2025-3-25 05:37:01
978-94-010-3836-2Springer Science+Business Media Dordrecht 2001
ONYM
发表于 2025-3-25 09:51:28
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吹牛大王
发表于 2025-3-25 14:01:07
0925-0042 Overview: 978-94-010-3836-2978-94-010-0724-5Series ISSN 0925-0042 Series E-ISSN 2214-7764
评论者
发表于 2025-3-25 18:53:42
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
发表于 2025-3-25 20:46:51
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
发表于 2025-3-26 01:40:44
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
发表于 2025-3-26 06:39:54
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暴行
发表于 2025-3-26 11:25:31
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煞费苦心
发表于 2025-3-26 14:40:23
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注射器
发表于 2025-3-26 19:48:19
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