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The origin of loads
Why that configuration?
Takeoff and climb
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adverse yaw aerodynamic aileron aircraft design airflow airfoil airframe airplane airspeed altitude amphibian angle approach aspect ratio autogyro aviation basic brake cabin center of gravity Cessna chapter climb configuration constant-speed propeller control surfaces conventional landing gear cost cowling crosswind cruising flight cruising speed deflection developed empty weight engine equipment flaps flight test flying ft/min fuel fuselage gross weight gust horizontal tail horsepower hull hydrofoil increase induced drag inlet installation landing gear level flight lift coefficient load factor main gear main wheels maximum noise nosewheel operation performance pilot plane powerplant pressure private aircraft production propeller reduce result retractable rudder runway safety sailplane seaplane shown in Fig single-engine stability stalling speed strut T-tail tail arm tail load tail surfaces takeoff thrust tricycle gear tricycle landing gear trim turbocharged vertical tail wing area