Introduction to Aircraft Aeroelasticity And Dynamic Loads - Couverture rigide

Wright, Jan Robert; Cooper, Jonathan Edward

Couverture rigide

ISBN 10 : 0470858400 ISBN 13 : 9780470858400

Editeur : Wiley-Blackwell, 2007

Synopsis

Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. * Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques.* Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift.* Includes up-to-date experimental methods and analysis.* Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.

A propos du livre

Quatrième de couverture

Aircraft performance is influenced significantly both byaeroelastic phenomena, arising from the interaction of elastic,inertial and aerodynamic forces, and by load variations resultingfrom flight and ground manoeuvres and gust / turbulence encounters.There is a strong link between aeroelasticity and loads, and thesetopics have become increasingly integrated in recent years. 

Introduction to Aircraft Aeroelasticity and Loads introduces thereader to the main principles involved in a wide range ofaeroelasticity and loads topics. Divided into three sections, thebook begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control. It goes on to describe simplifiedmodels to illustrate aeroelastic behaviour and aircraft responsebefore introducing more advanced methodologies. Finally, itexplains how industrial certification requirements foraeroelasticity and loads may be met and relates these to theearlier theoretical approaches used.

• Presents fundamentals of structural dynamics, aerodynamics,static and dynamic aeroelasticity, response and load calculationsand testing techniques.
  

• Covers performance issues related to aeroelasticity such asflutter, control effectiveness, divergence and redistribution oflift.
  

• Includes up–to–date experimental methods and analysis.
  

• Accompanied by a website with MatLAB and SIMULINK programs thatrelate to the models used.

• Introduction to Aircraft Aeroelasticity and Loads enables thereader to understand the aeroelastic and loads principles andprocedures employed in a modern aircraft design office. It willappeal to final year undergraduate and masters students as well asengineers who are new to the aerospace industry.
  

Revue de presse

"This book is a welcome addition to the aeroelastician′s armoury, as it brings the subject matter completely up–to–date, additionally adding a valuable and realistic industrial perspective." ( Aeronautical Journal, December 2008)

Détails de l'édition

• Éditeur: Wiley-Blackwell
• Date d'édition: 2007
• Langue: anglais
• ISBN 10: 0470858400
• ISBN 13: 9780470858400
• Reliure: Relié
• Nombre de pages: 526
• Coordonnées du fabricant: non disponible
• Personne responsable: non disponible