Airplane Design |
Contents
Discussion and Results | 2-26 |
Airplane Layout | 31 |
Vertical Location of Wing on Fuselage | 3-20 |
7 other sections not shown
Common terms and phrases
aileron airfoil airload airplane design angle of attack aspect ratio bending moments bicycle gear calculated center of gravity characteristics CLmax coefficient of lift condition critical cruising speed dCm/dCL decrease determined direct operating cost distance drag coefficient efficient equal Equation equilibrium feet field length flap deflected flight Fowler flap fuselage gravity location ground effect gust load factor horizontal tail increase induced drag jet transport landing gear lift coefficient lift curve Mach number maximum CL MCRD method mi/lb nacelle number of passengers obtained optimum altitude outboard outrigger parasite drag plan form plane presented propeller range rate of climb rear spar shear shown in Figure skin slope span spanwise specifications stringers structural sweepback and thickness sweptback wing tail surfaces take-off weight taper ratio thickness ratio thrust loading tion tires torsion box usually variation velocity vertical tail wing area wing loading wing weight zero