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A model of the Transonic Truss-Braced Wing aircraft in a wind tunnel at NASA's Ames Research Center. By early 2019, following extensive wind tunnel testing at NASA Ames Research Center, an optimized truss and more sweep for the 170 ft (52 m) span wing allowed flying higher and faster, up from Mach 0.70–0.75 to Mach 0.80 like current jetliners. [3]
"Electric aircraft generates buzz at Oshkosh air show". Chicago Tribune. August 1, 2010. "Air show examines hybrid airliners". United Press. Aug 2, 2010. "NASA, Boeing Test Low-Drag Truss-Braced Wing Concept: High-aspect-ratio, truss-braced wing promises marked fuel savings". Aviation Week & Space Technology. Aviation Week Network. January 27, 2014
The Henderson Longster is a conventional landing gear equipped, wire braced parasol wing aircraft. Aeronautical designer Ivan Diggs designed a new 30 ft wing for the Longster. [1] The wire bracing is supported by a central cabane post located over a 1 U.S. gallon (3.8 L; 0.83 imp gal) above-wing fuel tank. The fuselage is steel tubing.
The wings are strut-braced with a single spar and are made from fibreglass and foam with a 15.5% CAGI.R3 airfoil. The wing has a span of 31 .5 feet and an area of 127.4 sq ft (11.84 m 2), which gives it a wing loading of 9.5 lbs/sq ft at gross weight. The aircraft has removable wings, with single locking pins and quick-disconnect controls which ...
Data from Cliche and L'il Hustler General characteristics Crew: one Capacity: one passenger Length: 20 ft 6 in (6.25 m) Wingspan: 33 ft 6 in (10.21 m) Wing area: 172 sq ft (16.0 m 2) Empty weight: 500 lb (227 kg) Gross weight: 1,200 lb (544 kg) in the Canadian basic ultralight category, 1500 lbs in the amateur-built category. Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 ...
Data from Jane's All the World's Aircraft 1966/7, p.331, Aerofiles General characteristics Capacity: 1 Length: 16 ft 6 in (5.03 m) Upper wingspan: 19 ft 0 in (5.79 m) Lower wingspan: 18 ft 0 in (5.49 m) Height: 6 ft 0 in (1.83 m) Wing area: 110.0 sq ft (10.22 m 2) Aspect ratio: 6.33 Airfoil: NACA 4412 Empty weight: 700 lb (318 kg) Max takeoff weight: 1,247 lb (566 kg) Fuel capacity: 20 Imp gal ...
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The Low-Wing Longster is a single place, wire braced, low wing, open cockpit aircraft with conventional landing gear. The lower wing wire bracing is connected to the landing gear. The root wing ribs are oversized to create a smooth wing to fuselage fillet. The aircraft was the last in a series of homebuilt aircraft designs from Les Long.
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