journal article·2001-11

Simultaneous Active Damping and Health Monitoring of Aircraft Panels

Daniel J. Inman, Mehdi Ahmadian, Richard O. Claus

Publisher page

Abstract

The concept of using the same hardware to perform both structural health monitoring and control simultaneously is explored. Aircraft panels often require damping treatments in order to reduce fatigue. At the same time, manufacturers are starting to use health monitoring as a basis for maintenance. Here, an example of doing simultaneous health monitoring and control on a sample plate is presented as experimental evidence that both functions can be performed with the same set of hardware. In this case, smart materials, a piezoceramic patch (PZT) and a fiber optic sensor, are used as the common hardware.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Structural Health Monitoring Techniques · Ultrasonics and Acoustic Wave Propagation · Smart Materials for Construction

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Center for Intelligent Material Systems and Structures, Department of Mechanical Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061

Advanced Vehicle Dynamics Laboratory, Department of Mechanical Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061

Fiber and Electro-Optics Research Center, Departments of Electrical and Computer Engineering and of Materials Science and Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061

References (16)

Show source-provided references
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