Here is 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. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. Over one hundred illustrations and tables help clarify the text, while more than fifty problems enhance student learning.

1. Introduction 2. Structural dynamics 3. Static aeroelasticity 4. Aeroelastic flutter Bibliography Appendix A: Lagrange's equation Index.

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, First Edition, 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, First Edition, with Dewey H. Hodges (2002). --This text refers to an alternate Hardcover edition.

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