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...

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Detalles Bibliográficos
Autor principal: Roskam, Jan
Formato: Libro
Lenguaje:Inglés
Publicado: Lawrence : DAR Corporation, 1997, 2004.
Edición:2nd. print., 4th. print.
Colección:Airplane Design: Part II
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Aporte de:Registro referencial: Solicitar el recurso aquí
Descripción
Sumario: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.
Descripción Física:310 p. : il. ; 28 cm.
ISBN:1884885438