Health Monitoring of Aircraft Structures Using Piezoelectric Sensors: Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements - Softcover
The number of aging aircraft has increased in the recent years. In this situation new technologies of intensive integrated airframe damage monitoring without the involvement of additional man-hours are highly appreciated. This work represents an experimental research on some rudimentary elements of a potential structural health monitoring system which is based on piezoelectric sensors and exploits guided Lamb waves and electromechanical impedance as physical phenomenon for damage detection in aluminum aircraft thin walled structures. Two experimental research topics are briefly covered: guided Lamb waves feasibility regarding aluminum aircraft fatigue damage detection and electromechanical impedance feature application for piezoelectric sensor local stiffness variation detection, e.g. fatigue crack and joint tightness loss. The work includes some experiments on damage detection in the Mil Mi-8 helicopter tail boom structural elements.
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Sergey Kuznetsov obtained a doctoral degree in engineering science from the Riga Technical University in 2012.
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- PublisherLAP LAMBERT Academic Publishing
- Publication date2012
- ISBN 10 3659127558
- ISBN 13 9783659127557
- BindingPaperback
- Number of pages140
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors: Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
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Book Description Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The number of aging aircraft has increased in the recent years. In this situation new technologies of intensive integrated airframe damage monitoring without the involvement of additional man-hours are highly appreciated. This work represents an experimental research on some rudimentary elements of a potential structural health monitoring system which is based on piezoelectric sensors and exploits guided Lamb waves and electromechanical impedance as physical phenomenon for damage detection in aluminum aircraft thin walled structures. Two experimental research topics are briefly covered: guided Lamb waves feasibility regarding aluminum aircraft fatigue damage detection and electromechanical impedance feature application for piezoelectric sensor local stiffness variation detection, e.g. fatigue crack and joint tightness loss. The work includes some experiments on damage detection in the Mil Mi-8 helicopter tail boom structural elements. 140 pp. Englisch. Seller Inventory # 9783659127557
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors : Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
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Book Description Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The number of aging aircraft has increased in the recent years. In this situation new technologies of intensive integrated airframe damage monitoring without the involvement of additional man-hours are highly appreciated. This work represents an experimental research on some rudimentary elements of a potential structural health monitoring system which is based on piezoelectric sensors and exploits guided Lamb waves and electromechanical impedance as physical phenomenon for damage detection in aluminum aircraft thin walled structures. Two experimental research topics are briefly covered: guided Lamb waves feasibility regarding aluminum aircraft fatigue damage detection and electromechanical impedance feature application for piezoelectric sensor local stiffness variation detection, e.g. fatigue crack and joint tightness loss. The work includes some experiments on damage detection in the Mil Mi-8 helicopter tail boom structural elements. Seller Inventory # 9783659127557
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
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ISBN 13: 9783659127557
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors
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Book Description Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Kuznetsov SergeySergey Kuznetsov obtained a doctoral degree in engineering science from the Riga Technical University in 2012.The number of aging aircraft has increased in the recent years. In this situation new technologies of i. Seller Inventory # 5133370
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