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  2. General Electric F110 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F110

    The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace (formerly GE Aviation). It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well.

  3. Category:Ducted fan-powered aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Ducted_fan...

    Aircraft whose primary form of thrust is derived from a piston engine, rotary engine or turboshaft driving a ducted fan. Subcategories This category has the following 2 subcategories, out of 2 total.

  4. Diverterless supersonic inlet - Wikipedia

    en.wikipedia.org/wiki/Diverterless_supersonic_inlet

    The modified F-16 demonstrated a maximum speed of Mach 2.0 (Mach 2.0 is the F-16's clean certified maximum speed) and handling characteristics similar to a normal F-16. It was also shown that subsonic specific excess power was slightly improved. The DSI concept was introduced into the JAST/JSF program as a trade study item in mid-1994.

  5. Turbofan - Wikipedia

    en.wikipedia.org/wiki/Turbofan

    Rolls-Royce engines have a 72–82% propulsive efficiency and 42–49% thermal efficiency for a 0.63–0.49 lb/lbf/h (64,000–50,000 g/kN/h) TSFC at Mach 0.8, and aim for theoretical limits of 95% for open rotor propulsive efficiency and 60% for thermal efficiency with stoichiometric turbine entry temperature and 80:1 overall pressure ratio ...

  6. KAI T-50 Golden Eagle - Wikipedia

    en.wikipedia.org/wiki/KAI_T-50_Golden_Eagle

    T-50 Golden Eagle on a squadron flight. The T-50 program was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. [5]

  7. Propfan - Wikipedia

    en.wikipedia.org/wiki/Propfan

    The popularity of turbojets and turbofans curtailed research in propellers, but by the 1960s, interest increased when studies showed that an exposed propeller driven by a gas turbine could power an airliner flying at a speed of Mach 0.7–0.8 and at an altitude of 35,000 feet (11,000 metres). The term propfan was created during this period.

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