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Active Wave Propagation and Sensing in PlatesHealth monitoring of aerospace structures can be done using an active interrogation approach with diagnostic Lamb waves. Piezoelectric patches are often used to generate the waves, and it is helpful to understand how these waves propagate through a structure. To give a basic understanding of the actual physical process of wave propagation, a model is developed to simulate asymmetric wave propagation in a panel and to produce a movie of the wave motion. The waves can be generated using piezoceramic patches of any size or shape. The propagation, reflection, and interference of the waves are represented in the model. Measuring the wave propagation is the second important aspect of damage detection. Continuous sensors are useful for measuring waves because of the distributed nature of the sensor and the wave. Two sensor designs are modeled, and their effectiveness in measuring acoustic waves is studied. The simulation model developed is useful to understand wave propagation and to optimize the type of sensors that might be used for health monitoring of plate-like structures.
Document ID
20020009163
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ghoshal, Anindya
Martin, William N.
Sundaresan, Mannur J.
Schulz, Mark J.
Ferguson, Frederick
Date Acquired
September 7, 2013
Publication Date
September 14, 2001
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AD-A395622
Meeting Information
Meeting: Third Workshop on Structural Health Monitoring
Location: Stanford, CA
Country: United States
Start Date: September 12, 2001
End Date: September 14, 2001
Funding Number(s)
CONTRACT_GRANT: F49620-00-1-0232
CONTRACT_GRANT: NAG8-1646
CONTRACT_GRANT: DAAD19-00-1-0536
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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