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  2. Bagalini Bagaliante - Wikipedia

    en.wikipedia.org/wiki/Bagalini_Bagaliante

    The Bagaliante is constructed from wood and metal and is of pod-and-boom layout. [1]The 12.2 m (40.0 ft) span wing employs a Göttingen 535 airfoil at the wing root, transitioning to an NACA 4412 section at the wingtip.

  3. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    For example, the NACA 2412 airfoil has a maximum camber of 2% located 40% (0.4 chords) from the leading edge with a maximum thickness of 12% of the chord. The NACA 0015 airfoil is symmetrical, the 00 indicating that it has no camber. The 15 indicates that the airfoil has a 15% thickness to chord length ratio: it is 15% as thick as it is long.

  4. Template:Aircraft specs - Wikipedia

    en.wikipedia.org/wiki/Template:Aircraft_specs

    This template employs intricate features of template syntax. You are encouraged to familiarise yourself with its setup and parser functions before editing the template. If your edit causes unexpected problems, please undo it quickly, as this template may appear on a large number of pages.

  5. Explorer PG-1 Aqua Glider - Wikipedia

    en.wikipedia.org/wiki/Explorer_PG-1_Aqua_Glider

    The biplane wing employs a NACA 4412 airfoil. [2] [3] [4] The aircraft is towed behind a ski tow boat, lifting off at 35 mph (56 km/h) and climbing to about 200 ft (61 m), depending on the length of the tow rope used. The aircraft does not stall, but enters a nose-high mushing condition with a slow rate of descent. [3] [4]

  6. National Advisory Committee for Aeronautics - Wikipedia

    en.wikipedia.org/wiki/National_Advisory...

    NACA experience provided a model for World War II research, the postwar government laboratories, and NACA's successor, the National Aeronautics and Space Administration (NASA). NACA also participated in development of the first aircraft to fly to the "edge of space", North American's X-15. NACA airfoils are still used on modern aircraft.

  7. Clark Y airfoil - Wikipedia

    en.wikipedia.org/wiki/Clark_Y_airfoil

    The profile was designed in 1922 by Virginius E. Clark using thickness distribution of the German-developed Goettingen 398 airfoil. [1] The airfoil has a thickness of 11.7 percent and is flat on the lower surface aft of 30 percent of chord. The flat bottom simplifies angle measurements on propellers, and makes for easy construction of wings.

  8. NACA duct - Wikipedia

    en.wikipedia.org/wiki/NACA_duct

    A NACA duct, [1] also sometimes called a NACA scoop or NACA inlet, is a common form of low-drag air inlet design, originally developed by the U.S. National Advisory Committee for Aeronautics (NACA), the precursor to NASA, in 1945.

  9. Aeronautical Information Publication - Wikipedia

    en.wikipedia.org/wiki/Aeronautical_Information...

    These changes are received well in advance so that users of the aeronautical data can update their flight management systems . For insignificant changes, the published calendar dates are used. In some countries the AIP is informally known as the Airman's Manual or the Air Pilot.