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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 The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II General characteristics Crew: 1 Length: 6.25 m (20 ft 6 in) Wingspan: 12 m (39 ft 4 in) Height: 1.3 m (4 ft 3 in) at cockpit Wing area: 12 m 2 (130 sq ft) Aspect ratio: 12 Airfoil: Root – NACA 2418, Tip – NACA 2412, Mid – NACA 0012 Empty weight: 240 kg (529 lb) Gross weight: 357 kg (787 lb ...
Its 38.00 ft (11.6 m) span wing employs a NACA 2412 airfoil, mounts flaps and has a wing area of 181.00 sq ft (16.815 m 2). The acceptable power range is 200 to 250 hp (149 to 186 kW) and the standard engine used is the 230 hp (172 kW) Continental O-470 .
Burnelli's designs were based on the idea that an airfoil-section fuselage could contribute to the lift generated. ... General characteristics. Crew ... NACA 2412 [7 ...
Its 38.1 ft (11.6 m) extended-span wing employs a NACA 2412 airfoil, has an area of 191 sq ft (17.7 m 2) and mounts large Fowler flaps. The aircraft can be equipped with engines ranging from 200 to 350 hp (149 to 261 kW). The standard engine used is the 300 hp (224 kW) Continental IO-520 four-stroke powerplant.
Data from Jane's All The World's Aircraft 1955–56 General characteristics Crew: 1 Capacity: 3 passengers Length: 24 ft 11 + 1 ⁄ 2 in (7.607 m) Wingspan: 36 ft (11 m) Height: 6 ft 7 in (2.01 m) Wing area: 174 sq ft (16.2 m 2) Aspect ratio: 7.46:1 Airfoil: NACA 2412 Empty weight: 1,205 lb (547 kg) Gross weight: 2,200 lb (998 kg) Fuel capacity: 42 US gal (160 L; 35 imp gal) Powerplant: 1 × ...
Airfoil: Front wing: NACA 23018 at root, NACA 2412 at tip; Rear wing: NACA 23021 at root, NACA 2415 at tip; Empty weight: 2,405 lb (1,091 kg) Gross weight: 2,800 lb (1,270 kg) Fuel capacity: 25 imp gal (113.65 L) Sweepback on leading edge rear wing 21° 0′ 48″ Powerplant: 2 × de Havilland Gipsy Major IC inline piston engine, 140 hp (100 kW ...
General characteristics. Crew: 2; Length: 29 ft 3 in (8.92 m) ... Airfoil: NACA 2418 at root, NACA 2412 at tip; Empty weight: 4,056 lb (1,840 kg) Max takeoff weight: ...