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CRUISING WITH STABILITY
USEFUL LOAD AND WEIGHT CONTROL
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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 Chap coefficient configuration constant speed propeller control surfaces conventional landing gear cost crosswind cruising flight cruising speed deflection developed effect efficiency engine equipment FIGURE flaps flight test flying ft/min fuel fuselage gross weight gust horizontal tail horsepower hull hydrofoil increase induced drag installation landing gear level flight lift lift coefficient load factor main gear main wheels maneuvering maximum noise nosewheel operation percent performance pilot plane powerplant pressure private aircraft 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 tion tricycle gear tricycle landing gear trim turbocharged vertical tail wing area