Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System

Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System 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