Preliminary configuration design and integration of the propulsion system /
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Lawrence, Kansas :
DARcorporation,
impresión 2004, ©1985.
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| Series: |
Airplane design
2 |
| Subjects: | |
| Notas Contenido: |
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Table of Contents:
- 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
