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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors: Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements - Softcover
Synopsis
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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About the Author
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
- LanguageEnglish
- Number of pages140
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors
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LAP LAMBERT Academic Publishing Mai 2012, 2012
ISBN 10: 3659127558
ISBN 13: 9783659127557
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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
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
Quantity: 2 available
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors : Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
Published by
LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659127558
ISBN 13: 9783659127557
New
Taschenbuch
Seller: AHA-BUCH GmbH, Einbeck, Germany
Seller rating 5 out of 5 stars
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
Quantity: 1 available
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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors
Published by
LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659127558
ISBN 13: 9783659127557
New
Softcover
Seller: moluna, Greven, Germany
Seller rating 5 out of 5 stars
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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Health Monitoring of Aircraft Structures Using Piezoelectric Sensors: Integrated piezoceramic sensors for damage detection in aluminum aircraft structural elements
Published by
LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659127558
ISBN 13: 9783659127557
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Paperback
Seller: Mispah books, Redhill, SURRE, United Kingdom
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Paperback. Condition: Like New. Like New. book. Seller Inventory # ERICA79636591275586
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