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Suboptimal Controllers For Reduction Of Vibration And Sound Radiation - Softcover

 
9783330077850: Suboptimal Controllers For Reduction Of Vibration And Sound Radiation

Synopsis

Vibration control of flexible structures is an important issue in many engineering applications. As large lightweight structures used in the aeronautical and space fields are characterized by modal frequencies and damping ratios relatively low, they are widely affected by vibrations that may cause problems both in terms of safety and comfort. Structural vibration can cause structure-borne noise to the structure, which is especially critical to aerospace structure and underwater vehicle such as commercial aircraft or submarine system.The transmission of acoustic noise is one of the main issues and the improvement of the flight comfort trying to reduce radiated noise produced by the vibrating structures of the airplane represents an important challenge in civil aeronautics. Therefore, to comply with the request of vibration suppression and noise attenuation, the concept of actively controlled structures with sensors and actuators has to be introduced. In recent years, several studies have been conducted on active control, both using piezoelectric and inertial actuators .

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About the Author

Anurag Tiwari was born in India. In 2013, he received a bachelors degree in Aerospace Engineering from Amity University, India. He has a masters degree in Space Engineering from Politecnico di Milano, Italy, year 2016 . His work related to Manned mission to Mars has been published in two international space conferences.

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  • PublisherLAP LAMBERT Academic Publishing
  • Publication date2017
  • ISBN 10 3330077859
  • ISBN 13 9783330077850
  • BindingPaperback
  • LanguageEnglish
  • Number of pages64

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ISBN 10: 3330077859 ISBN 13: 9783330077850
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Vibration control of flexible structures is an important issue in many engineering applications. As large lightweight structures used in the aeronautical and space fields are characterized by modal frequencies and damping ratios relatively low, they are widely affected by vibrations that may cause problems both in terms of safety and comfort. Structural vibration can cause structure-borne noise to the structure, which is especially critical to aerospace structure and underwater vehicle such as commercial aircraft or submarine system.The transmission of acoustic noise is one of the main issues and the improvement of the flight comfort trying to reduce radiated noise produced by the vibrating structures of the airplane represents an important challenge in civil aeronautics. Therefore, to comply with the request of vibration suppression and noise attenuation, the concept of actively controlled structures with sensors and actuators has to be introduced. In recent years, several studies have been conducted on active control, both using piezoelectric and inertial actuators . 64 pp. Englisch. Seller Inventory # 9783330077850

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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Vibration control of flexible structures is an important issue in many engineering applications. As large lightweight structures used in the aeronautical and space fields are characterized by modal frequencies and damping ratios relatively low, they are widely affected by vibrations that may cause problems both in terms of safety and comfort. Structural vibration can cause structure-borne noise to the structure, which is especially critical to aerospace structure and underwater vehicle such as commercial aircraft or submarine system.The transmission of acoustic noise is one of the main issues and the improvement of the flight comfort trying to reduce radiated noise produced by the vibrating structures of the airplane represents an important challenge in civil aeronautics. Therefore, to comply with the request of vibration suppression and noise attenuation, the concept of actively controlled structures with sensors and actuators has to be introduced. In recent years, several studies have been conducted on active control, both using piezoelectric and inertial actuators . Seller Inventory # 9783330077850

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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tiwari AnuragAnurag Tiwari was born in India. In 2013, he received a bachelors degree in Aerospace Engineering from Amity University, India. He has a masters degree in Space Engineering from Politecnico di Milano, Italy, year 2016 . . Seller Inventory # 151236733

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