Introduction to Aircraft Aeroelasticity and Loads
Wright, Jan Robert; Cooper, Jonathan Edward
Language: English
Published by Wiley, 2008
Series: Book 74 of 125 - AIAA Education
- Hardcover
- Used
Seller: Blue Planet Textbooks, Keizer, OR, U.S.A.Blue Planet Textbooks
AbeBooks seller since June 16, 2017
Condition: Used - Good
£ 188.30
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Add to basketSeller Inventory # 52f410944367389b91d14fcf405a0d3f
- Title
- Introduction to Aircraft Aeroelasticity and Loads
- Author
- Wright, Jan Robert; Cooper, Jonathan Edward
- Publisher
- Wiley
- Publication year
- 2008
- Condition
- Good
- Binding
- Hardcover
- Language
- English
- ISBN 10
- 0470858400
- ISBN 13
- 9780470858400
- Series
- Book 74 of 125: AIAA Education
Introduction to Aircraft Aeroelasticity and Loadsintroduces the reader to the main principles involved in a widerange of aeroelasticity and loads topics. Divided into threesections, the book begins by reviewing the underlying disciplinesof vibrations, aerodynamics, loads and control. It goes on todescribe simplified models to illustrate aeroelastic behaviour andaircraft response before introducing more advanced methodologies.Finally, it explains 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 enablesthe reader 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.
"Synopsis" may belong to another edition of this title.
From the Back Cover
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.
"About the title" may belong to another edition of this title.
Blue Planet Textbooks
Keizer, OR, U.S.A.
AbeBooks seller since June 16, 2017
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