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

by Jan Roskam

Airplane Design Part 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 Preliminary Configuration Design and Integration of the Propulsion System familiarizes the reader with the following - 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

324 pages, Paperback

First published January 1, 1999

Reviews

[Agus]

good education