Proyecto: Evaluación y configuración de los Sistemas Piloto Automático Micropilot (31852-33694) Contents: Chapter 1: Introduction. --Chpater 2: Review of practical aerodynamics. p. 33.--Chpater 3: Aircraf performance methods. p. 71.--Chpater 4: Aircraf operating envelope. p. 101.--Chapter 5: Prelimininary estimate of takeoff weight. p. 123.--Chapter 6: Estimating the takeoff wing loading. p. 151.--Chpater 7: Slecting the planform and airfoils section. p. 171.--Chapter 8: Preliminary fuselage sizing and design. p. 195.--Chapter 9: High-lift devices. p. 221.--Chapter 10: Takeoff and landing analysis. p. 255.--Chapter 11: Preliminary sizing of the vertical and horizontal tails. p. 283.--Chpater 12: Designing for survivability (Stealth), p. 293.--Chapter 13: Estimating wing-body aerodynamics. p. 323.--Chapter 14: Propulsion systems fundamentals. p. 355.--Chapter 15: Turbne engine inlet design. p. 383.--Chpater 16: Corrections for turbine engine installation. p. 413.--Chpater 17; Propeller propulsion systems. p. 435.--Chapter 18: Prpoulsion systems thurst sizing. p. 467.--Chapter 19: Structures and materials. p. 491.--Chapter 20: Refined weight estimate. p. 551.--Chapter 21: Static stability an control. p. 575.--Chapter 22: Trim drag and maneuvering flight. p. 601.--Chapter 23: Control surface sizing criteria. p. 613.--Chapter 24: Life cycle cost. p. 625.--Chapter 25: Tarde Studies and sizing. p. 651
