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Descriptive Design Procedure
Relations for the Airplane Performance and Design Nomogram
l S WS W Wing Area Wing Loading Gross Weight
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Aerodynamics aircraft airfoil airplane efficiency factor Airplane Performance airspeed angle of attack Appendix F boundary layer brake horsepower Calculation for Relation CL,minS decreases density altitude density ratio Design Nomogram Figure Dimensionless Dmin drag area effective aspect ratio effective chord effective span loading Effectivel engine brake equation flaps fuselage glide angle gross weight ground effect ideal climb rate ideal rate increase induced drag L/Dlmax level flight speed Lpading maximum level flight maximum lift coefficient maximum lift-to-drag ratio Minimum Drag minimum sink rate nomogram in Figure parasite drag Performance and Design performance rating parameter propeller diameter propeller efficiency propeller tip Mach rate of climb reference point required for level Reynolds number RS,min sample calculation sea level sink rate curve stall speed THPmin tip Mach number turbocharged velocity Vmax Vmins Vprop W/be wing area wing loading zero-lift drag coefficient