Search results
Results from the WOW.Com Content Network
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 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 ...
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.
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.
Data from Jane's All the World's Aircraft 1969–70 General characteristics Crew: one Capacity: one passenger Length: 22 ft 8 in (6.91 m) Wingspan: 33 ft 5 in (10.19 m) Height: 6 ft 7 + 3 ⁄ 4 in (2.03 m) Wing area: 165 sq ft (15.3 m 2) Aspect ratio: 6.72:1 Airfoil: NACA 4412 Empty weight: 1,037 lb (470 kg) Gross weight: 1,650 lb (748 kg) Fuel capacity: 39 US gal (32 imp gal; 150 L ...
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]
Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!
Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 Length: 18 ft 0 in (5.49 m) Wingspan: 24 ft 0 in (7.32 m) Height: 5 ft 1.5 in (1.562 m) Wing area: 100 sq ft (9.3 m 2) Airfoil: NACA 4412 Empty weight: 440 lb (200 kg) Max takeoff weight: 750 lb (340 kg) Powerplant: 1 × Volkswagen 4-cylinder air-cooled horizontally-opposed piston engine, 40 hp (30 kW ...