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" Introduction to aircraft aeroelasticity and loads / "
Jan R. Wright, Jonathan E. Cooper.
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BL
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| Record Number
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997295
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b751665
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| Main Entry
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Wright, Jan R.
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| Title & Author
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Introduction to aircraft aeroelasticity and loads /\ Jan R. Wright, Jonathan E. Cooper.
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| Publication Statement
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Chichester, England ;Hoboken, NJ :: John Wiley,, ©2007.
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| Series Statement
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Aerospace series
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| Page. NO
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1 online resource (xxiv, 499 pages) :: illustrations.
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| ISBN
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0470858400
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: 0470858419
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: 047085846X
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: 6611319778
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: 9780470858400
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: 9780470858417
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: 9780470858462
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: 9786611319779
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0470858478
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9780470858479
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| Bibliographies/Indexes
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Includes bibliographical references (pages 491-493) and index.
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| Contents
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pt. I. Background Material -- 1. Vibration of Single Degree of Freedom Systems -- 2. Vibration of Multiple Degree of Freedom Systems -- 3. Vibration of Continuous Systems -- Assumed Shapes Approach -- 4. Vibration of Continuous Systems -- Discretization Approach -- 5. Introduction to Steady Aerodynamics -- 6. Introduction to Loads -- 7. Introduction to Control -- pt. II. Introduction to Aeroelasticity and Loads -- 8. Static Aeroelasticity -- Effect of Wing Flexibility on Lift Distribution and Divergence -- 9. Static Aeroelasticity -- Effect of Wing Flexibility on Control Effectiveness -- 10. Introduction to Unsteady Aerodynamics -- 11. Dynamic Aeroelasticity -- Flutter -- 12. Aeroservoelasticity -- 13. Equilibrium Manoeuvres -- 14. Flight Mechanics Model for Dynamic Manoeuvres -- 15. Dynamic Manoeuvres -- 16. Gust and Turbulence Encounters -- 17. Ground Manoeuvres -- 18. Aircraft Internal Loads -- 19. Potential Flow Aerodynamics -- 20. Coupling of Structural and Aerodynamic Computational Models -- pt. III. Introduction to Industrial Practice -- 21. Aircraft Design and Certification -- 22. Aeroelasticity and Loads Models -- 23. Static Aeroelasticity and Flutter -- 24. Flight Manoeuvre and Gust/Turbulence Loads -- 25. Ground Manoeuvre Loads -- 26. Testing Relevant to Aeroelasticity and Loads -- App. A. Aircraft Rigid Body Modes -- App. B. Table of Longitudinal Aerodynamic Derivatives -- App. C. Aircraft Symmetric Flexible Modes -- App. D. Model Condensation.
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| Abstract
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Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.
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| Subject
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Aeroelasticity.
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| Subject
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Aeroelasticity.
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TRANSPORTATION-- Aviation-- General.
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| Dewey Classification
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629.134/1
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| LC Classification
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TL574.A37W75 2007eb
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| Added Entry
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Cooper, Jonathan E.
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