Roskam, Jan. <br/><br/>
Airplane design. Part II :   Preliminary configuration design and integration of the propulsion system 

 - 2nd. print., 4th. print. 
 - Lawrence :   DAR Corporation,   1997, 2004. 
 - 310 p. :   il. ;   28 cm. 
 - Airplane Design: Part II .
<br/><br/> 1- Introduction. 2- Step-by step guide to configuration design. 3- Selection of the overall configuration. 4- Design of cockpit and fuselage layouts. 5- Selection and integration of the propulsion. 6- Class I method for wing palnform design and for sizing and locating lateral control surfaces. 7- Class I method for verifying clean airplane and for sizing high lift devices. 8- Class I method for empennage sizing and disposition and for control surface sizing and disposition. 9- Class I method for landing gear sizing and disposition. 10- Class I weight and balance analysis. 11- Class I method for stability and control analysis. 12- Class I method for drag polar determination. 13- The result of preliminary design sequenceI: the preliminary threeview. 
<br/><br/><label>ISBN: </label>1884885438 
<br/><br/><label>Subjects--Topical Terms: </label><br/>SISTEMA DE PROPULSION<br/>SUPERFICIES DE CONTROL<br/>PESO Y BALANCEO<br/>DISEŅO PRELIMINAR<br/>DISEŅO DE LA PLANTA ALAR<br/>DISPOSITIVO HIPERSUSTENTADOR<br/>SUPERFICIES DE CONTROL<br/>TREN DE ATERRIZAJE
<br/><br/><label>Universal Decimal Class. No.: </label>629.7.01