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:
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

MARC

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100 1 |a Roskam, Jan,  |d 1930-  |e autor 
245 1 0 |a Preliminary configuration design and integration of the propulsion system /  |c Jan Roskam. 
260 |a Lawrence, Kansas :  |b DARcorporation,  |c impresión 2004, ©1985. 
300 |a 310 páginas :  |b ilustraciones en blanco y negro ;  |c 29 cm. 
490 0 |a Airplane design  |v 2 
500 |a Incluye referencias bibliográficas e índice 
505 0 |a 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 
650 1 7 |a Sistemas de propulsión  |2 Armarc 
650 2 7 |a Peso y balance  |2 Tesauro especializado en aviación 
650 2 7 |a Aviones a reacción  |2 Armarc 
650 1 7 |a Aviones  |x Diseño y construcción  |2 Armarc 
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