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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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