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BASIC DESIGN CONSIDERATIONS
THE ORIGIN OF LOADS
THE SEARCH FOR UTILITY
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adverse yaw aerodynamic aileron aircraft design airflow airfoil airframe airplane airspeed altitude amphibian angle of attack approach aspect ratio autogyro aviation basic cabin carburetor center of gravity Cessna Chap chord climb rate configuration constant speed propeller control surfaces cost cowling crosswind cruising flight cruising speed developed drag coefficient effect efficiency empty weight engine equipment fixed pitch flap flight speed flight test flying ft/min fuel fuselage gross weight gust horizontal tail horsepower hull improved increase induced drag inlet installation landing gear level flight lift coefficient load factor maximum noise nosewheel operation percent performance pilot plane powerplant pressure private aircraft reduce result retractable rudder runway safety sailplane sea-level seaplane shown by Fig stability stalling speed strut T-tail tail arm tail load tail surfaces thrust tion tricycle gear trim turbocharged vertical tail wing area