Airplane design. Part II : Preliminary configuration design and integration of the propulsion system
Tipo de material:
TextoSeries Airplane Design: Part IIDetalles de publicación: Lawrence : DAR Corporation, 1997, 2004.Edición: 2nd. print., 4th. printDescripción: 310 p. : il. ; 28 cmISBN: - 1884885438
Libro
| Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
|---|---|---|---|---|---|
| Koha Ingenieria | 629.7.01 ROS II-Bloque 19 (Navegar estantería(Abre debajo)) | Disponible | A2664 | ||
| Koha Ingenieria | 629.7.01 ROS II-Bloque 19 (Navegar estantería(Abre debajo)) | Disponible | 37995 |
Navegando Koha Ingenieria estanterías Cerrar el navegador de estanterías (Oculta el navegador de estanterías)
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| 629.7.01 ROS I-Bloque 19 Airplane Design. Part I : Preliminary sizing of airplanes | 629.7.01 ROS I-Bloque 19 Airplane Design. Part I : Preliminary sizing of airplanes | 629.7.01 ROS II-Bloque 19 Airplane design. Part II : Preliminary configuration design and integration of the propulsion system | 629.7.01 ROS II-Bloque 19 Airplane design. Part II : Preliminary configuration design and integration of the propulsion system | 629.7.01 ROS III-Bloque 19 Airplane Design. Part III : Layout design of cockpit, fuselage, wing and empennage: cutaways and inboard profiles | 629.7.01 ROS III-Bloque 19 Airplane Design. Part III : Layout design of cockpit, fuselage, wing and empennage: cutaways and inboard profiles | 629.7.01 ROS IV Bloque 19 Airplane Design : Part IV: Layout Design of Landing Gear and Systems. |
1- Introduction. 2- Step-by step guide to configuration design. 3- Selection of the overall configuration. 4- Design of cockpit and fuselage layouts. 5- Selection and integration of the propulsion. 6- Class I method for wing palnform design and for sizing and locating lateral control surfaces. 7- Class I method for verifying clean airplane and for sizing high lift devices. 8- Class I method for empennage sizing and disposition and for control surface sizing and disposition. 9- Class I method for landing gear sizing and disposition. 10- Class I weight and balance analysis. 11- Class I method for stability and control analysis. 12- Class I method for drag polar determination. 13- The result of preliminary design sequenceI: the preliminary threeview.
A2664 COMP
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