Airplane design. Part II : Preliminary configuration design and integration of the propulsion system
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- Cl...
Guardado en:
| Autor principal: | |
|---|---|
| Formato: | Libro |
| Lenguaje: | Inglés |
| Publicado: |
Lawrence :
DAR Corporation,
1997, 2004.
|
| Edición: | 2nd. print., 4th. print. |
| Colección: | Airplane Design: Part II
|
| Materias: | |
| Aporte de: | Registro referencial: Solicitar el recurso aquí |
| LEADER | 01974cam#a22003853a#4500 | ||
|---|---|---|---|
| 001 | INGC-MON-09845 | ||
| 003 | AR-LpUFI | ||
| 005 | 20221019003902.0 | ||
| 008 | 060510s1997 |||a fr||||| |0 0|eng d | ||
| 020 | |a 1884885438 | ||
| 080 | |a 629.7.01 | ||
| 100 | 0 | |a Roskam, Jan. |9 282986 | |
| 245 | 0 | 0 | |a Airplane design. Part II : |b Preliminary configuration design and integration of the propulsion system |
| 250 | |a 2nd. print., 4th. print. | ||
| 260 | |a Lawrence : |b DAR Corporation, |c 1997, 2004. | ||
| 300 | |a 310 p. : |b il. ; |c 28 cm. | ||
| 440 | 0 | 0 | |a Airplane Design: Part II |9 284489 |
| 520 | 2 | |a 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. | |
| 599 | |a A2664 COMP | ||
| 650 | 1 | 4 | |a SISTEMA DE PROPULSION |9 283851 |
| 650 | 1 | 4 | |a SUPERFICIES DE CONTROL |9 283867 |
| 650 | 1 | 4 | |a PESO Y BALANCEO |9 284304 |
| 650 | 1 | 4 | |a DISEÑO PRELIMINAR |9 284490 |
| 650 | 1 | 4 | |a DISEÑO DE LA PLANTA ALAR |9 284491 |
| 650 | 1 | 4 | |a DISPOSITIVO HIPERSUSTENTADOR |9 283949 |
| 650 | 1 | 4 | |a SUPERFICIES DE CONTROL |9 283867 |
| 650 | 1 | 4 | |a TREN DE ATERRIZAJE |9 281560 |
| 929 | |a A2664 COM; 37995 DON Canal | ||
| 942 | |c LIB |6 _ | ||
| 959 | |a MON | ||
| 960 | |a 10532 | ||
| 970 | |a Registro convertido en forma automatizada | ||
| 990 | |a GBY | ||
| 999 | |c 9843 |d 9843 | ||
| 040 | |a AR-LpUFI |c AR-LpUFI | ||