E-grāmata: Introduction to Aeroelasticity

James DeLaurier

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Other book format (Cena: -) - 01-Dec-2024

Formāts: 196 pages
Izdošanas datums: 30-Dec-2024
Izdevniecība: CRC Press
Valoda: eng
ISBN-13: 9781040223390

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Formāts: 196 pages
Izdošanas datums: 30-Dec-2024
Izdevniecība: CRC Press
Valoda: eng
ISBN-13: 9781040223390

Citas grāmatas par šo tēmu:

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"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. This book is intended to be a quantitative survey course for senior undergraduate or graduate students, as well as any engineer wishing a thorough introduction to the topic. Instructors will be able to utilize a Solutions Manual and Figure Slides for their course based upon this book"--

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.

James DeLaurier has worked as an aerospace engineer, consultant, and professor. He received his PhD from Stanford University and has worked at McDonnell Aircraft, the NASA Ames Research Center, the Sheldahl Company, and Battelle Memorial Institute. Until his retirement in 2006, Dr. DeLaurier was a professor at the University of Toronto Institute for Aerospace Studies (UTIAS). His research topics have included aircraft design, lighter-than-air flight vehicles (airships and aerostats), flapping-wing aircraft, and remotely-piloted microwave-powered aircraft.

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