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  2. T-tail - Wikipedia

    en.wikipedia.org/wiki/T-tail

    T-tails were common in early jet aircraft. Designers were worried that an engine failure would otherwise damage the horizontal tail. The T-tail is very common on aircraft with engines mounted in nacelles on a high-winged aircraft or on aircraft with the engines mounted on the rear of the fuselage, as it keeps the tail clear of the jet exhaust.

  3. Stall (fluid dynamics) - Wikipedia

    en.wikipedia.org/wiki/Stall_(fluid_dynamics)

    Normal flight (above), Deep stall condition - T-tail in "shadow" of wing (below) A Schweizer SGS 1-36 being used for deep-stall research by NASA over the Mojave Desert in 1983. A deep stall (or super-stall) is a dangerous type of stall that affects certain aircraft designs, notably jet aircraft with a T-tail configuration and rear-mounted ...

  4. AASI Jetcruzer - Wikipedia

    en.wikipedia.org/wiki/AASI_Jetcruzer

    The AASI Jetcruzer was an American single turboprop light civil transport made by Advanced Aerodynamics and Structures Inc. The Jetcruzer had an unusual configuration, with a single turboprop engine driving a pusher propeller, a prominent canard, and fins mounted at the ends of its swept wings. The plane has seating for up to six people ...

  5. Empennage - Wikipedia

    en.wikipedia.org/wiki/Empennage

    T-tail – The horizontal stabiliser is mounted on top of the fin, creating a "T" shape when viewed from the front. T-tails keep the stabilisers out of the engine wake, and give better pitch control. T-tails have a good glide ratio, and are more efficient on low speed aircraft. However, the T-tail has several disadvantages.

  6. Aircraft flight mechanics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_mechanics

    Aircraft flight mechanics are relevant to fixed wing (gliders, aeroplanes) and rotary wing (helicopters) aircraft.An aeroplane (airplane in US usage), is defined in ICAO Document 9110 as, "a power-driven heavier than air aircraft, deriving its lift chiefly from aerodynamic reactions on surface which remain fixed under given conditions of flight".

  7. Aerodynamically alleviated marine vehicle - Wikipedia

    en.wikipedia.org/wiki/Aerodynamically_alleviated...

    The advantages of this new configuration come from the aerodynamic lift. The additional aerodynamic lift can be equal to the 30-80% of the total weight of the marine vehicle. This means a lower hydrodynamic lift needed, therefore a lower chine and keel wetted length and a decreased hydrodynamic drag.

  8. Why don’t humans have tails? Scientists find answers in an ...

    www.aol.com/why-don-t-humans-tails-093029995.html

    Even if the driving mutation identified in the study could be undone, “it still wouldn’t bring back the tail.” The new findings may also shed light on a type of neural tube defect in embryos ...

  9. Pitch-up - Wikipedia

    en.wikipedia.org/wiki/Pitch-up

    In aircraft with high-mounted tailplanes, like the F-101 Voodoo, recovery was especially difficult because the tailplane was placed directly in the wing wake during the pitch-up, causing deep stall (although the T-tail was meant to prevent pitch-up from starting in the first place). Deployment of the braking parachute and a considerable height ...