raja samikkannu (6 risultati)

Paperback. Condizione: Brand New. 268 pages. 8.66x5.91x0.61 inches. In Stock.

Taschenbuch. Condizione: Neu. Adaptive Structures with Vibration Control Applications | Samikkannu Raja | Taschenbuch | 268 S. | Englisch | 2016 | LAP LAMBERT Academic Publishing | EAN 9783659978432 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.

Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Vibration control is a useful technique for aerospace, mechanical and automotive systems. This can be accomplished either by active or passive vibration control techniques. Active control system needs distributed actuators, sensors and processor. Piezoelectric materials can be employed as actuators and sensors in adaptive structures for structural control applications. The present book addresses the modelling techniques of piezoelectric materials with multi-field coupling and their use in distributed active vibration control of laminated composite sandwich beams, plates and shells. Finite Element formulations are derived in detail with suitable validation studies. Control schemes are explained in a simplified manner, so that graduate students, research scholars and practising engineers can adopt active control concepts easily in their works. Finally the real time vibration control applications in aerospace structures are presented to highlight the technology related implementation issues. 268 pp. Englisch.

Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Raja SamikkannuHolding MTech and PhD in Aerospace Engineering and working as Senior Principal Scientist in CSIR-National Aerospace Laboratories, India. Awarded DAAD research and JSPS post-doctoral fellowships. Published 60 papers in .

Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Vibration control is a useful technique for aerospace, mechanical and automotive systems. This can be accomplished either by active or passive vibration control techniques. Active control system needs distributed actuators, sensors and processor. Piezoelectric materials can be employed as actuators and sensors in adaptive structures for structural control applications. The present book addresses the modelling techniques of piezoelectric materials with multi-field coupling and their use in distributed active vibration control of laminated composite sandwich beams, plates and shells. Finite Element formulations are derived in detail with suitable validation studies. Control schemes are explained in a simplified manner, so that graduate students, research scholars and practising engineers can adopt active control concepts easily in their works. Finally the real time vibration control applications in aerospace structures are presented to highlight the technology related implementation issues.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 268 pp. Englisch.

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Vibration control is a useful technique for aerospace, mechanical and automotive systems. This can be accomplished either by active or passive vibration control techniques. Active control system needs distributed actuators, sensors and processor. Piezoelectric materials can be employed as actuators and sensors in adaptive structures for structural control applications. The present book addresses the modelling techniques of piezoelectric materials with multi-field coupling and their use in distributed active vibration control of laminated composite sandwich beams, plates and shells. Finite Element formulations are derived in detail with suitable validation studies. Control schemes are explained in a simplified manner, so that graduate students, research scholars and practising engineers can adopt active control concepts easily in their works. Finally the real time vibration control applications in aerospace structures are presented to highlight the technology related implementation issues.