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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.
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 15.0 m (49.2 ft) span wing features top and bottom air brakes and employs NACA 63-618 airfoil at the wing root, and a NACA 4412 section at the wing tip. The controls are automatically connected on assembly. The bubble canopy slides aft for cockpit access and can be locked open in several positions in flight. The landing gear is a fixed ...
Data from Sport Aviation. General characteristics Capacity: 2 Length: 19 ft 7 in (5.97 m) Wingspan: 26 ft (7.9 m) Wing area: 130 sq ft (12 m 2) Airfoil: NACA 4412 Empty weight: 820 lb (372 kg) Gross weight: 1,300 lb (590 kg) Fuel capacity: 21 US gal (79 L) Powerplant: 1 × Continental C85-12F or Lycoming O-235/O-290, 85–135 hp (63–101 kW) Propellers: 2-bladed Performance Maximum speed: 130 ...
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 ...
Data from Jane's All The World's Aircraft 1966–67, [1] ... Airfoil: NACA 23024 at root, NACA 4412 at tip; Empty weight: 1,034 kg (2,280 lb) equipped;
Data from Fighting Gliders of World War II, [3] United States Military Aircraft: ... Airfoil: root: NACA 23018; tip: NACA 4412 [5] Empty weight: 12,150 lb (5,511 kg)
Its 9.15 m (30.0 ft) span wing employs a NACA 4415 airfoil at the wing root, transitioning to a NACA 4412 at the wing tip. The wing has an area of 11.3 m 2 (122 sq ft) and mounts flaps. Standard engines available are the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. The ...