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J Chapter 4 Airfoil and Geometry Selection
Chapter 5 ThrusttoWeight Ratio and Wing Loading
Chapter 6 Initial Sizing
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actual aerodynamic aerodynamic center aileron aircraft design aircraft weight airflow airfoil altitude analysis angle of attack approximately aspect ratio calculated camber canard Chapter chord climb component compression Conceptual Approach conceptual design cost cross section cruise curve deflection determined dihedral duct dynamic pressure effect empty weight engine equations estimated fighter flap flight flow force fuel fuselage horizontal tail increase induced drag initial inlet landing gear layout leading-edge lift coefficient lift force load factor longitudinal Mach number maximum lift methods MISSION SEGMENT nacelle nozzle parasite drag pilot pitching produce propeller propulsion reduced roll shear shock shown in Fig sizing specific fuel consumption speed stall static structural subsonic supersonic surface T-tail takeoff weight thrust tion transonic turboprop turn rate typical usually vectoring velocity vertical tail VTOL wave drag weight fraction wetted area wheel wing loading zero