TY  - BOOK
T1  - Airplane design. Part II : Preliminary configuration design and integration of the propulsion system
T2  - Airplane Design: Part II
A1  - Roskam, Jan
LA  - English
PP  - Lawrence
PB  - DAR Corporation
YR  - 1997
ED  - 2nd. print., 4th. print.
UL  - http://vufind10-pruebas.sigbunlp.bibliotecas.unlp.edu.ar/Record/dfi.9843
AB  - 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.
OP  - 310
SN  - 1884885438
KW  - SISTEMA DE PROPULSION
KW  - SUPERFICIES DE CONTROL
KW  - PESO Y BALANCEO
KW  - DISEÑO PRELIMINAR
KW  - DISEÑO DE LA PLANTA ALAR
KW  - DISPOSITIVO HIPERSUSTENTADOR
KW  - TREN DE ATERRIZAJE
ER  -