ISBN13: | 9781032709062 |
ISBN10: | 1032709065 |
Binding: | Hardback |
No. of pages: | 198 pages |
Size: | 234x156 mm |
Language: | English |
Illustrations: | 138 Illustrations, black & white; 6 Halftones, black & white; 132 Line drawings, black & white; 12 Tables, black & white |
700 |
Applied mathematics
Engineering in general
Mechanical Engineering Sciences
Civil and construction engineering
Traffic engineering sciences, automotive and transportation industry
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Mechanics
Air transport
Applied mathematics (charity campaign)
Engineering in general (charity campaign)
Mechanical Engineering Sciences (charity campaign)
Civil and construction engineering (charity campaign)
Traffic engineering sciences, automotive and transportation industry (charity campaign)
Environmental sciences (charity campaign)
Mechanics (charity campaign)
Air transport (charity campaign)
Introduction to Aeroelasticity
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This book introduces the classical topics of aeroelasticity, beginning with elastic structural modeling and the way that wing and tail structures can diverge and deform due to aerodynamic, inertial, and control-surface deflections. It presents equation derivations in a step-by-step fashion, complemented by numerical and historical examples.
Introduction to Aeroelasticity introduces the classical topics of aeroelasticity, beginning with elastic structural modeling and the way that wing and tail structures can diverge and deform due to aerodynamic, inertial, and control-surface deflections.
After describing flutter, first with an airfoil example with increasing complexity, and then for flutter predictions of finite wings with and without control surfaces, the book expands into single-degree-of-freedom flutter. It introduces cable ?galloping,? Aeolian flutter, plunging and pitching stall flutter. The book presents equation derivations in a step-by-step fashion, complemented by several numerical and historical examples.
The book is intended for senior undergraduate and graduate aerospace engineering students taking introductory courses in Aeroelasticity.
Instructors will be able to utilize a Solutions Manual and Figure Slides for their course.
1. Introduction. 2. Structural Aspects: Stiffness and Flexibility. 3. Divergence. 4. Control Reversal. 5. Structural Dynamics. 6. Classical Flutter. 7. Single-Degree of Freedom Flutter. Appendix A. Lumped-Parameter Coupled Bending and Twisting. Appendix B. Flutter of the Representative Section with Control Surface.