Introduction to Aeroelasticity
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Product details:
- Edition number 1
- Publisher CRC Press
- Date of Publication 30 December 2024
- ISBN 9781032709062
- Binding Hardback
- No. of pages196 pages
- Size 234x156 mm
- Weight 453 g
- Language English
- Illustrations 138 Illustrations, black & white; 6 Halftones, black & white; 132 Line drawings, black & white; 12 Tables, black & white 675
Categories
Short description:
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.
MoreLong description:
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.
Flutter is then described, first with an airfoil example with increasing complexity, and then for flutter predictions of finite wings with and without control surfaces.Single-degree-of-freedom flutter is also discussed, which includes cable ?galloping,? Aeolian flutter, as well as plunging and pitching stall flutter. In all cases, the equation derivations proceed in a step-by-step fashion, complemented by several numerical (and historical) examples.
The book is intended to be a quantitative survey course for senior undergraduate and graduate students, as well as any engineer wishing a thorough introduction of the topic.
Instructors will be able to utilize a Solutions Manual and figure slides for their course based upin this book.
MoreTable of Contents:
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.
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