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afterburner - device attached at exit of jet engine exhaust pipe to burn unburned fuel and exhaust gases, thus producing added thrust
aileron - hinged or movable control surface, usu. on trailing edge of wing near tip, that regulates banking by causing movement about longitudinal axis
air brake - airfoil that can be extended to produce additional drag for slowing aircraft
airfoil - any surface, esp. wing, designed to produce a useful reaction when properly positioned in airstream
airframe - any part of aircraft other than engine: fuselage, booms, nacelle, cowlings, fairings, airfoils, landing gear
fuselage - elongated main body of airplane housing engines, crew, cargo, passengers, and equipment
gas turbine - propulsion engine using hot, compressed gas as working fluid, consisting of compressor, combustion chamber, and turbine through which expanded gases are discharged to drive compressor and propel aircraft
gondola - cabin suspended under airship or balloon for passengers and engine
gull wing - wing that slants upward from fuselage for short distance, then levels out
honeycomb - sandwich panel used for airplane skins: thin outer layers of metal, wood, or plastic with honeycomb core of metal, plastic, or paper for lightness and strength
horizontal stabilizer - stabilizer mounted horizontally in tail assembly, to which elevators are attached for lateral stability
horn - short lever fastened to control surface, to which operating cable or rod is attached
supercharger - engine-driven compressor that increases flow of air and fuel into cylinders to improve power in nonjet engines and maintains pressure in cabin and engine
sweep - fore-and-aft angle of airfoil relative to fuselage
sweepback - wing with leading edge at sharp angle to fuselage; swept-back wing
tail wheel - small wheel that supports tail of aircraft with conventional landing gear on ground
throat - most constricted part of jet exhaust nozzle; inlet
throttle - hand-operated lever connected to valve that controls amount of fuel delivered to engine cylinders; fuel control for gas turbines in jet engines
thrust chamber - chamber of jet engine, in which combustion of fuel and air, or oxidizer, takes place
thrust spoiler - jet device used to reduce forward thrust without decreasing mass flow from engine
truss - assembly of structural members forming rigid framework for fuselage
turbine - rotary engine with drive shaft powered by action of liquid or gas against curved vanes of wheel or escaping through nozzles located around wheel
turbofan - turbojet engine that creates additional thrust by diverting secondary airflow around combustion chamber; fanjet engine
turbojet - jet engine supplied with air from compressor driven by turbine that is activated by energy of jet exhaust gases
turboprop - variation of turbojet in which gas turbine also drives conventional propeller to produce major portion of thrust; propjet
turret - transparent dome for gunner on bomber or fighter