Engineering:Nuri Demirağ Nu D.36
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Short description: Turkish trainer aircraft
| Nu D.36 | |
|---|---|
| |
| Nuri Demirag Nu.D.36 | |
| Role | Two-seat training biplane |
| National origin | Turkey |
| Manufacturer | Nuri Demirağ Aircraft Works |
The Nuri Demirağ Nu D.36 was a 1930s Turkish two-seat training biplane built by the Nuri Demirağ Aircraft Works in Istanbul for the Turkish military.
Design
The Nu D.36 is an unequal-span single-bay staggered biplane with a fixed conventional landing gear with a tailskid. It was powered by a 150 hp (112 kW) Walter Gemma I nine-cylinder radial engine. It had two open tandem cockpits for the pilot and trainee.
Operators
Turkey
Specifications
Data from Jane's Fighting Aircraft of World War II,[1] Jane's all the World's Aircraft 1947[2]
General characteristics
- Crew: 2
- Length: 7.3 m (23 ft 11 in)
- Wingspan: 9.74 m (31 ft 11 in)
- Height: 2.44 m (8 ft 0 in)
- Wing area: 21.8 m2 (235 sq ft)
- Empty weight: 650 kg (1,433 lb)
- Max takeoff weight: 1,000 kg (2,205 lb)
- Powerplant: 1 × Walter Gemma I 9-cyl. air-cooled radial piston engine, 110 kW (150 hp)
- Propellers: 2-bladed fixed pitch wooden propeller
Performance
- Maximum speed: 182 km/h (113 mph, 98 kn)with maximum load
<--*Landing speed: 85 km/h (53 mph; 46 kn) (commented out as this does not work in wikitext) -->
- Range: 500 km (310 mi, 270 nmi)
- Endurance: 3 hours 30 minutes
- Service ceiling: 3,350 m (10,990 ft)
- Time to altitude: 500 m (1,600 ft) in 2 minutes; 1,500 m (4,900 ft) in 10 minutes
References
- ↑ Bridgman, Leonard (1988). Jane's Fighting Aircraft of World War II. New York: Crescent Books. p. 200. ISBN 0-517-67964-7.
- ↑ Bridgman, Leonard, ed (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. p. 174c.
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