Introduction to Structural Dynamics and Aeroelasticity
Seiten
2002
Cambridge University Press (Verlag)
978-0-521-80698-5 (ISBN)
Cambridge University Press (Verlag)
978-0-521-80698-5 (ISBN)
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This text provides 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. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.
Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides 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. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.
Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides 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. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.
1. Introduction; 2. Structural dynamics; 3. Static aeroelasticity; 4. Aeroelastic flutter; Bibliography; Appendix A: Lagrange's equation; Index.
| Erscheint lt. Verlag | 1.7.2002 |
|---|---|
| Reihe/Serie | Cambridge Aerospace Series |
| Zusatzinfo | Worked examples or Exercises; 17 Tables, unspecified; 41 Line drawings, unspecified |
| Verlagsort | Cambridge |
| Sprache | englisch |
| Maße | 182 x 263 mm |
| Gewicht | 502 g |
| Themenwelt | Technik ► Fahrzeugbau / Schiffbau |
| Technik ► Luft- / Raumfahrttechnik | |
| Technik ► Maschinenbau | |
| ISBN-10 | 0-521-80698-4 / 0521806984 |
| ISBN-13 | 978-0-521-80698-5 / 9780521806985 |
| Zustand | Neuware |
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