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Introduction to Structural Dynamics and Aeroelasticity: 15 (Cambridge Aerospace Series, Series Number 15) - Softcover
Synopsis
This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft.
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About the Authors
Dewey H. Hodges is a professor in the School of Aerospace Engineering at the Georgia Institute of Technology. He is the author of more than 170 refereed journal papers and three books, Nonlinear Composite Beam Theory (2006), Fundamentals of Structural Stability, with G. J. Simitses (2005) and Introduction to Structural Dynamics and Aeroelasticity, with G. Alvin Pierce (2002). His research spans the fields of aeroelasticity, dynamics, computational structural mechanics and structural dynamics, perturbation methods, computational optimal control and numerical analysis.
The late G. Alvin Pierce was Professor Emeritus in the School of Aerospace Engineering at the Georgia Institute of Technology. He was the co-author of Introduction to Structural Dynamics and Aeroelasticity, with Dewey H. Hodges (2002).
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- PublisherCambridge University Press
- Publication date2014
- ISBN 10 110761709X
- ISBN 13 9781107617094
- BindingPaperback
- LanguageEnglish
- Edition number2
- Number of pages272
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity
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Cambridge University Press, 2014
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ISBN 13: 9781107617094
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Introduction to Structural Dynamics and Aeroelasticity
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ISBN 10: 110761709X
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity (Cambridge Aerospace Series, Series Number 15)
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity
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Introduction to Structural Dynamics and Aeroelasticity (Paperback)
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ISBN 10: 110761709X
ISBN 13: 9781107617094
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Paperback. Condition: new. Paperback. This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than one hundred illustrations and tables help clarify the text and more than fifty problems enhance student learning. This text meets the need for an up-to-date treatment of structural dynamics and aeroelasticity for advanced undergraduate or beginning graduate aerospace engineering students. This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft. It considers structural dynamics, static aeroelasticity and dynamic aeroelasticity. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than fifty problems enhance student learning. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Seller Inventory # 9781107617094
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