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Airpalne Design, Part II : Preliminary Configuration design and Integration
Airpalne Design, Part II : Preliminary Configuration design and Integration
Author: Roskam, Jan
Edition/Copyright: 1997
ISBN: 1-884885-43-8
Publisher: DARcorporation
Type: Paperback
New Print:  $42.00 Used Print:  $31.50
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Summary
 
  Summary

This is the second book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference. Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System, familiarizes the reader with the following fundamentals:

  • Selection of the overall configuration
  • Design of cockpit and fuselage layouts
  • Selection and integration of the propulsion system
  • Class I method for wing planform design
  • Class I method for verifying clean airplane maximum lift coefficient and for sizing high lift devices
  • Class I method for empennage sizing and disposition, control surface sizing and disposition, landing gear sizing and disposition, weight and balance analysis, stability and control analysis and drag polar determination
 

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