Preliminary configuration design and integration of the propulsion system /

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Bibliographic Details
Main Author:	Roskam, Jan (autor)
Format:	Book
Language:	English
Published:	Lawrence, Kansas : DARcorporation, impresión 2004, ©1985.
Series:	Airplane design 2
Subjects:	Sistemas de propulsión Peso y balance Aviones a reacción Aviones > Diseño y construcción
Notas Contenido:	Step-by-step guide to configuration desing Selection os the overall configuration Desing of cockpit and fuselage layounts Selection and integration os the propulsion system Class I method for wing plataform desing and for sizing and locating lateral control surfaces Class I method for verifying clean airplane CLmax and for sizing high lift devices Class I method for empennage sizing and disposition and for control surface sizong and disposition Class I method for landing gear sizing ans disposition Class I weight and balance analysis Class I method for stability and control analñisys Class I method for drag polar determination The result of preliminary desing sequence I: the preliminary threeview

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Call Number:	629.13435 R821p
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