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Airplane Design Part II Preliminary Configuration Design and Integration of the Propulsion System
Free Download Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System By Jan Roskam1997 | 310 Pages | ISBN: 1884885438 | PDF | 14 MB
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
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