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  2. 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.

  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. Aeronautical Information Publication - Wikipedia

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

    In this respect, a digital AIP is a digital version of the paper AIP, usually available in PDF format, while an electronic AIP is available in PDF as well as other formats, more suitable for reading on the screen and for electronic data exchange. Many countries around the world provide digital AIPs either on CD-ROM subscription or on a Web site.

  5. NACA duct - Wikipedia

    en.wikipedia.org/wiki/NACA_duct

    The Ferrari F40 sports car has "NACA style" side and hood scoops.. It is especially favored in racing car design. [4] [5] Sports cars featuring prominent NACA ducts include the Ferrari F40, the Lamborghini Countach, the 1996–2002 Dodge Viper, the 1971–1973 Ford Mustang, the 1973 Pontiac GTO, the 1979 Porsche 924 Turbo, the Maserati Biturbo, the Nissan S130, and the Porsche 911 GT2.

  6. 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.

  7. Robert Thomas Jones (engineer) - Wikipedia

    en.wikipedia.org/wiki/Robert_Thomas_Jones_(engineer)

    In January 1945, Jones developed a theory of the delta wing based on thin-airfoil theory. Others at Langley were sceptical until supersonic testing of models was done by Robert Gilruth and in April by Theodore von Karman. Jones's theory was not truly accepted until that summer when Von Karman's team of investigators found that German experts ...

  8. PZL-Mielec M-18 Dromader - Wikipedia

    en.wikipedia.org/wiki/PZL-Mielec_M-18_Dromader

    PZL-Mielec, then known as WSK-Mielec, began to design the Dromader in the mid 1970s, with help of United States aircraft manufacturer Rockwell International.PZL-Mielec asked for Rockwell's help because of the political situation at the time: operating in an Eastern Bloc country, PZL wanted the aircraft to sell well worldwide, and the company realized that certification by the United States ...

  9. NACA score - Wikipedia

    en.wikipedia.org/wiki/NACA_score

    A NACA score (or National Advisory Committee for Aeronautics score) is a scoring system of the severity in cases of medical emergencies such as injuries, diseases or poisonings. It was developed from the National Advisory Committee for Aeronautics for accidents in aviation.