Aircraft design : a conceptual approach /
Design-A separate discipline - Overview of the design process - Sizing from a conceptual sketch - Airfoil and wing/tail geometry selection - Trust-to-wight ratio and wing loading - Initial sizing - Configuration layout and loft - Special considerations in configuration layout - Crew station, passeng...
Guardado en:
| Autor principal: | |
|---|---|
| Formato: | Libro |
| Lenguaje: | Inglés |
| Publicado: |
Virginia :
American Institute of Aeronautics and Astronautics,
2012.
|
| Edición: | 5th ed. |
| Colección: | AIAA Education
|
| Materias: | |
| Aporte de: | Registro referencial: Solicitar el recurso aquí |
| LEADER | 01429Cam#a22002295a#4500 | ||
|---|---|---|---|
| 001 | INGC-MON-018558 | ||
| 003 | AR-LpUFI | ||
| 005 | 20230908093134.0 | ||
| 008 | 140307s2012||||xxu|||||||||||||||||eng d | ||
| 020 | |a 9781600869112 | ||
| 040 | |a AR-LpUFI |b spa |c AR-LpUFI | ||
| 080 | |a 629.7.01 | ||
| 100 | 1 | |a Raymer, Daniel P. |9 285093 | |
| 245 | 1 | 0 | |a Aircraft design : |b a conceptual approach / |c Daniel P. Raymer. |
| 250 | |a 5th ed. | ||
| 260 | |a Virginia : |b American Institute of Aeronautics and Astronautics, |c 2012. | ||
| 300 | |a xxviii, 1044 p. : |b tablas, figuras | ||
| 490 | |a AIAA Education | ||
| 520 | 2 | |a Design-A separate discipline - Overview of the design process - Sizing from a conceptual sketch - Airfoil and wing/tail geometry selection - Trust-to-wight ratio and wing loading - Initial sizing - Configuration layout and loft - Special considerations in configuration layout - Crew station, passengers and payload - Propulsion and fuel system integration - Landing gear and subsystems - Step-by-step development of a new design - Aerodynamics - Propulsion - Structures and loads - Weights - Stability, control and handling qualities - Performance and flight mechanics - Cost analysis - Sizing and trade studies - Vertical flight-jet and prop - Extremes of flight - Design of unique aircraft concepts - Conceptual design examples - Appendices. | |
| 650 | 4 | |a DISEÑO DE AERONAVES |9 272447 | |
| 942 | |c LIB |6 _ | ||
| 999 | |c 18557 |d 18557 | ||