Cargando…
Introduction to Aircraft Flight Mechanics.
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston :
American Institute of Aeronautics and Astronautics,
2000.
|
| Colección: | AIAA education series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Acknowledgments""; ""Chapter 1. A Review of Basic Aerodynamics""; ""Chapter 2. A Review of Basic Propulsion""; ""Chapter 3. Aircraft Performance""; ""Chapter 4. Aircraft Equations of Motion""; ""Chapter 5. Aircraft Static Stability""; ""Chapter 6. Linearizing the Equations of Motion""; ""Chapter 7. Aircraft Dynamic Stability""; ""Chapter 8. Classical Feedback Control""; ""Chapter 9. Aircraft Stability and Control Augmentation""; ""Appendix A. Conversions""
- ""Appendix B. Properties of the U.S. Standard Atmosphere""""Appendix C. Airfoil Data""; ""Appendix D. T-38 Performance Data""; ""Appendix E. Selected Laplace Transforms""; ""Appendix F. Cramer�s Rule""; ""Appendix G. Development of Longitudinal and Lateral�Directional Transfer Functions""; ""Appendix H. Stability Characteristics of Selected Aircraft""; ""Bibliography""; ""Index""; ""Series listing""