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Synopsis
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some 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.
Key features of this new edition include:
- Uses a unified simple aeroelastic model throughout the book
- Major revisions to chapters on aeroelasticity
- Updates and reorganisation of chapters involving Finite Elements
- Some reorganisation of loads material
- Updates on certification requirements
- Accompanied by a website containing a solutions manual, and MATLAB® and SIMULINK® programs that relate to the models used
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.
"synopsis" may belong to another edition of this title.
About the Author
Jan R. Wright
University of Manchester, UK
Jonathan E. Cooper
University of Bristol, UK
From the Back Cover
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some 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.
Key features of this new edition include:
• Uses a unified simple aeroelastic model throughout the book
• Major revisions to chapters on aeroelasticity
• Updates and reorganization of chapters involving Finite Elements
• Some reorganization of loads material
• Updates on certification requirements
• Accompanied by a website containing a solutions manual, and MATLAB® and SIMULINK® programs that
relate to the models used
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.
From the Inside Flap
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some 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.
Key features of this new edition include:
- Uses a unified simple aeroelastic model throughout the book
- Major revisions to chapters on aeroelasticity
- Updates and reorganization of chapters involving Finite Elements
- Some reorganization of loads material
- Updates on certification requirements
- Accompanied by a website containing a solutions manual, and MATLAB(R) and SIMULINK(R) programs that
relate to the models used
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.
"About this title" may belong to another edition of this title.
- PublisherWiley
- Publication date2015
- ISBN 10 1118488016
- ISBN 13 9781118488010
- BindingHardcover
- LanguageEnglish
- Edition number2
- Number of pages576
- Rating
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Hardcover. Condition: new. Hardcover. Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some 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. Key features of this new edition include: Uses a unified simple aeroelastic model throughout the bookMajor revisions to chapters on aeroelasticityUpdates and reorganisation of chapters involving Finite ElementsSome reorganisation of loads materialUpdates on certification requirementsAccompanied by a website containing a solutions manual, and MATLAB and SIMULINK programs that relate to the models used Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering. Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Seller Inventory # 9781118488010
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