• Thumbnail for Drag-reducing aerospike
    A drag-reducing aerospike is a device (see nose cone design) used to reduce the forebody pressure aerodynamic drag of blunt bodies at supersonic speeds...
    5 KB (520 words) - 15:53, 23 December 2024
  • rocket nozzle Drag-reducing aerospike, a device which reduces drag on missiles by creating a detached shock above the missile Aerospike cone, a jet engine...
    479 bytes (96 words) - 22:32, 24 March 2025
  • Thumbnail for Inlet cone
    P-500 Bazalt anti-ship missile Index of aviation articles Aerospike engine Drag-reducing aerospike Nose cone design Splitter plate NASA Dryden[permanent dead...
    10 KB (1,484 words) - 23:00, 23 February 2025
  • Thumbnail for Ram air turbine
    compliant wing Anti-shock body Blown flap Channel wing Dog-tooth Drag-reducing aerospike Flap Gouge flap Gurney flap Krueger flap Leading-edge cuff Leading-edge...
    12 KB (1,375 words) - 06:11, 17 June 2025
  • Thumbnail for Aerospike engine
    of aerospikes seem to be extra weight for the spike. Furthermore, the larger cooled area can reduce performance below theoretical levels by reducing the...
    25 KB (2,812 words) - 02:12, 5 June 2025
  • Thumbnail for Drogue parachute
    Drogue parachute (redirect from Drag chute)
    A drogue parachute, also called drag chute, is a parachute designed for deployment from a rapidly moving object. It can be used for various purposes, such...
    19 KB (1,790 words) - 02:35, 23 February 2025
  • Thumbnail for Conventional landing gear
    "rudder bar" in World War I—the skid pivoted to the right, creating more drag on that side of the plane and causing it to turn to the right. While less...
    14 KB (1,726 words) - 10:33, 14 April 2025
  • Thumbnail for Landing gear
    operation on land. Retractable undercarriages fold away during flight, which reduces drag, allowing for faster airspeeds. Landing gear must be strong enough to...
    88 KB (10,960 words) - 03:23, 17 June 2025
  • Thumbnail for Flap (aeronautics)
    aircraft. Flaps are used to reduce the take-off distance and the landing distance. Flaps also cause an increase in drag so they are retracted when not...
    32 KB (4,059 words) - 18:26, 16 June 2025
  • Thumbnail for Wingtip device
    by reducing drag. Although there are several types of wing tip devices which function in different manners, their intended effect is always to reduce an...
    45 KB (4,713 words) - 20:49, 7 June 2025
  • Thumbnail for Altimeter
    compliant wing Anti-shock body Blown flap Channel wing Dog-tooth Drag-reducing aerospike Flap Gouge flap Gurney flap Krueger flap Leading-edge cuff Leading-edge...
    6 KB (732 words) - 10:07, 21 May 2025
  • Thumbnail for Nacelle
    design issue with aircraft-mounted nacelles is streamlining to minimise drag so nacelles are mounted on slender pylons. This can cause issues with directing...
    7 KB (750 words) - 04:12, 6 June 2025
  • Thumbnail for Stabilizer (aeronautics)
    the outer wing sweep is reduced, so increasing drag, while the inner wing sweep increases, reducing drag. This change in the drag distribution creates a...
    21 KB (2,406 words) - 00:22, 13 June 2025
  • Thumbnail for V-tail
    exhaust, reducing thrust and increasing wear on the stabilizer, possibly leading to damage over time. In military aircraft, V-tails reduce the number...
    10 KB (1,083 words) - 14:18, 28 May 2025
  • Thumbnail for Ice protection system
    dangerous. Aircraft icing increases weight and drag, decreases lift, and can decrease thrust. Ice reduces engine power by blocking air intakes. When ice...
    15 KB (1,835 words) - 21:58, 9 January 2025
  • Thumbnail for Flight recorder
    making them much more resistant to shock, vibration and moisture. With the reduced power requirements of solid-state recorders, it is now practical to incorporate...
    74 KB (7,430 words) - 10:26, 15 June 2025
  • Thumbnail for Vortex generator
    an aircraft wing at high speed has a small angle of attack, thereby reducing VG drag to a minimum. Owners have reported that on the ground, it can be harder...
    12 KB (1,456 words) - 00:43, 24 January 2025
  • Thumbnail for T-tail
    "end plate" effect. The horizontal stabilizer acts like a winglet, reducing induced drag of the rudder. Smaller and lighter T-tails are often used on modern...
    9 KB (1,120 words) - 10:30, 2 May 2025
  • Thumbnail for Leading-edge slat
    German aircraft commonly fitted a more advanced version of the slat that reduced drag by being pushed back flush against the leading edge of the wing by air...
    11 KB (1,394 words) - 23:30, 26 March 2025
  • Thumbnail for Wing warping
    of discrete curvature changes and of gaps has the potential of reducing the shape drag associated to the wing, thus increasing their aerodynamic efficiency...
    9 KB (1,126 words) - 04:24, 18 March 2025
  • Thumbnail for High-lift device
    will provide more lift and reduce the distance and speeds required for takeoff and landing, but will increase drag, which reduces performance during the cruising...
    9 KB (1,252 words) - 14:07, 27 February 2025
  • Thumbnail for Elevator (aeronautics)
    of lift) situated aft of the airplane's center of gravity. The effects of drag and changing the engine thrust may also result in pitch moments that need...
    9 KB (942 words) - 04:33, 11 March 2024
  • Thumbnail for Flight control surfaces
    right amount of positive or negative lift from the tail plane while reducing drag from the elevators. A control horn is a section of control surface which...
    23 KB (2,876 words) - 14:59, 14 June 2025
  • Thumbnail for Stabilator
    from reduced drag, particularly at high Mach numbers, it is a useful device for changing the aircraft balance within wide limits, and for reducing stick...
    9 KB (1,111 words) - 07:59, 12 March 2025
  • Thumbnail for Vertical stabilizer
    vertical stabilizer as a way to disrupt the airflow to the rear wing reducing drag, the most radical system being the "F-duct" found in the 2010 McLaren...
    26 KB (3,388 words) - 00:12, 29 May 2025
  • Thumbnail for Drop tank
    is that they impose a drag penalty on the aircraft. External fuel tanks will also increase the moment of inertia, thereby reducing roll rates for air maneuvers...
    16 KB (1,969 words) - 06:04, 21 April 2025
  • Thumbnail for Self-sealing fuel tank
    tank, when hit by gunfire, could leak fuel rapidly. This would not only reduce the aircraft's range but was also a significant fire hazard. Damaged fuel...
    13 KB (1,372 words) - 17:58, 4 May 2025
  • Thumbnail for Servo tab
    the airflow deflection of the control surface. This has the effect of reducing the control force required from the pilot to move the controls.: 612  In...
    8 KB (887 words) - 13:42, 2 June 2025
  • Thumbnail for UGM-96 Trident I
    UGM-96 Trident I (C4) The first launch of a Trident I with a drag-reducing aerospike, from Cape Canaveral, on 18 January 1977 Type SLBM Place of origin...
    3 KB (220 words) - 01:35, 17 May 2025
  • Thumbnail for Tricycle landing gear
    nosewheel. Also, a fixed-gear taildragger exhibits less interference drag and form drag in flight than a fixed-gear tricycle aircraft whose nosewheel may...
    6 KB (737 words) - 13:07, 8 December 2024