Imagen de Google Jackets

Airplane design. Part V : Component weight estimation.

Por:

Roskam, Jan

Tipo de material: Texto

TextoSeries Airplane Design: Part VDetalles de publicación: Kansas : DARcorporation, 1989, 2003.Edición: 2nd. print., 3th. printDescripción: 209 p. + errata 8 p. : il. ; 28 cmISBN:

1884885500

Tema(s):

Resumen: Introduction. 2- Class I method for estimating airplane component weights. 3- Class I method for estimating airplane inertias. 4- Class II method for estimating airplane component weights. 5- Class II Method for estimating structure weight. 6- Class II method for estimating powerplant weight. 7- Class II method for estimating fixed equipment weight. 8- Locating component centers of gravity. 9- Class II weight and balance analysis. 10- Clas II method for estimating airplane inertias.

Tipo de ítem:

Libro

Existencias
Biblioteca actual	Signatura topográfica	Estado	Fecha de vencimiento	Código de barras
Koha Ingenieria	629.7.01 ROS V-Bloque 19 (Navegar estantería(Abre debajo))	Disponible		A2682
Koha Ingenieria	629.7.01 ROS V-Bloque 19 (Navegar estantería(Abre debajo))	Disponible		37998

Navegando Koha Ingenieria estanterías Cerrar el navegador de estanterías (Oculta el navegador de estanterías)

Previo		No hay imagen de cubierta disponible	No hay imagen de cubierta disponible					Siguiente
Previo	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.	629.7.01 ROS IV Bloque 19 Airplane Design : Part IV: Layout Design of Landing Gear and Systems.	629.7.01 ROS V-Bloque 19 Airplane design. Part V : Component weight estimation.	629.7.01 ROS V-Bloque 19 Airplane design. Part V : Component weight estimation.	629.7.01 ROS VI-Bloque 19 Airplane Design. Part VI : Preliminary calculation of aerodynamic, thrust and power characteristics	629.7.01 ROS VI-Bloque 19 Airplane Design. Part VI : Preliminary calculation of aerodynamic, thrust and power characteristics	Siguiente

Introduction. 2- Class I method for estimating airplane component weights. 3- Class I method for estimating airplane inertias. 4- Class II method for estimating airplane component weights. 5- Class II Method for estimating structure weight. 6- Class II method for estimating powerplant weight. 7- Class II method for estimating fixed equipment weight. 8- Locating component centers of gravity. 9- Class II weight and balance analysis. 10- Clas II method for estimating airplane inertias.

Tomo:V Ubic.:629.7.01 ROS Ej.1 PRES

No hay comentarios en este titulo.

para colocar un comentario.