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Fundamentals of aircraft and airship design /
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
Ã2010-
|
| Colección: | AIAA educational series.
|
| Temas: | |
| Acceso en línea: | Texto completo Texto completo |
Tabla de Contenidos:
- v. 1. Aircraft design. Introduction ; Review of practical aerodynamics ; Aircraft performance methods ; Aircraft operating envelope ; Preliminary estimate of takeoff weight ; Estimating the takeoff wing loading ; Selecting the planform and airfoil section ; Preliminary fuselage sizing and design ; High-lift devices ; Takeoff and landing analysis ; Preliminary sizing of the vertical and horizontal tails ; Designing for survivability (stealth) ; Estimating wing-body aerodynamics ; Propulsion system fundamentals ; Turbine engine inlet design ; Corrections for turbine engine installation ; Propeller propulsion systems ; Propulsion system thrust sizing ; Structures and materials ; Refined weight estimate ; Static stability and control ; Trim drag and maneuvering flight ; Control surface sizing criteria ; Life cycle cost ; Trade studies and sizing
- Appendix A : Conversions
- Appendix B : Atmospheric data
- Appendix C : Isentropic compressible flow functions
- Appendix D : Normal shock functions for a perfect gas
- Appendix E : Plane oblique and conical shocks
- Appendix F : NACA airfoil nomenclature and data
- Appendix G : Aerodynamic data of real aircraft
- Appendix H : Aerodynamics of wing-body combinations
- Appendix I : Aircraft weights data
- Appendix J : Propulsion data
- Appendix K : Miscellaneous data.