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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.
Data from Sport Aviation, original drawings, and Wickham B POH (Pilot Operating Handbook) Rev 3/18/06. General characteristics Capacity: 5 Length: 25 ft 10 in (7.87 m) Wingspan: 40 ft 3 in (12.27 m) Height: 9 ft 10 in (3.00 m) Wing area: 163 sq ft (15.1 m 2) Aspect ratio: 9.5 Airfoil: NACA 63A- 418, taper to 4412 Empty weight: 2,065 lb (937 kg) Gross weight: 3,200 lb (1,451 kg) Fuel capacity ...
The airfoil is a NACA laminar flow type of varying section over the span, starting at the wing root as a NACA 64(3)-618, becoming a NACA 64(3)-615 by mid-span and then a NACA 4412 at the tip. The wing is constructed from plywood and fiberglass and is responsible for the Annebula's performance increase from the Cherokee II's 23:1 glide ratio to ...
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.
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.
The semi-tapered wing was of 51 ft (15.5 m) span and used a NACA 63-518 wing root airfoil, transitioning to a NACA 4412 airfoil at the wing tip. The three-piece wing, with a fixed center section and removable tips, featured a foam-filled leading edge and large-sized lower surface dive brakes. The aircraft had a conventional tail with a tall ...
It was the brainchild of Al Meyers and was a development of his Meyers MAC-145 design. The holder of a number of speed records in its class, the Meyers 200 is widely admired for its clean lines, and is also known for its exceptionally sturdy airframe.
The Bell X-2 (nicknamed "Starbuster" [1]) was an X-plane research aircraft built to investigate flight characteristics in the Mach 2–3 range. The X-2 was a rocket-powered, swept-wing research aircraft developed jointly in 1945 by Bell Aircraft Corporation, the United States Army Air Forces and the National Advisory Committee for Aeronautics (NACA) to explore aerodynamic problems of ...