| Description |
1 online resource (xi, 173 pages) |
| Contents |
Front Cover; Contents; Preface; Author; 1. Introduction; 2. Elementary Aerodynamics; 3. Static Aeroelasticity; 4. Divergence of a Lifting Surface; 5. Divergence of a Typical Section with a Control Surface; 6. Dynamic Aeroelasticity; 7. One-Dimensional Aeroelastic Model of Airfoils; 8. Rolling of a Straight Wing; 9. Flutter of a Cantilever Wing; 10. Approximate Techniques of Modeling Continuous Systems; 11. Nonlinear Aeroelasticity; 12. Unsteady Aerodynamics; References; Back Cover |
| Summary |
Introductory Guide on the Design of Aerospace Structures Developed from a course taught at Concordia University for more than 20 years, Principles of Aeroelasticity utilizes the author's extensive teaching experience to immerse undergraduate and first-year graduate students into this very specialized subject. Ideal for coursework or self-study, this detailed examination introduces the concepts of aeroelasticity, describes how aircraft lift structures behave when subjected to aerodynamic loads, and finds its application in aerospace, civil, and mechanical engineering |
| Bibliography |
Includes bibliographical references and index |
| Notes |
Print version record |
| Subject |
Aeroelasticity.
|
|
TECHNOLOGY & ENGINEERING -- Engineering (General)
|
|
Aeroelasticity
|
| Form |
Electronic book
|
| ISBN |
9781498724739 |
|
1498724736 |
|
9781523107025 |
|
1523107022 |
|
