A Practical Guide to Airplane Performance and Design |
Contents
Idealized Propeller Theory | 2 |
Summary of the Nomogram Calculation for the T18 | 71 |
Parametric Study of the Baseline Design | 82 |
Copyright | |
10 other sections not shown
Common terms and phrases
20 Chord 2000 Span Loading 600 Maximum Power Aerodynamics aircraft airfoil airplane efficiency factor Airspeed for 74 Airspeed Vmins angle of attack Appendix F CD,O CL,max decreases density altitude density ratio Design Nomogram Figure Dmin drag area effective aspect ratio effective chord effective span loading Engine Brake Horsepower equation flaps ft² fuselage Gossamer Albatross Gossamer Condor Gross Weight ground effect ideal climb rate Idealized Maximum induced drag lb/ft level flight speed Lift/Drag Ratio L/D)max Mach Number Mp maximum level flight maximum lift coefficient maximum lift-to-drag ratio Minimum Power Required minimum sink rate parasite drag Performance and Design performance rating parameter prop Propeller Diameter Dp Propeller Tip Mach rate of climb RC,max required for level Reynolds number RS,min sample calculation stall speed THPa THPmin Tip Mach Number Turbocharged Vmax W/be wing area Wing Loading Zero-Lift Drag Coefficient سلسل ليلي