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LWD Żuraw

From Wikipedia, the free encyclopedia
1950s Polish utility aircraft
LWD Żuraw
Damaged prototype in thePolish Aviation Museum
RoleLiaison aircraft
Type of aircraft
ManufacturerLWD
First flight16 May 1951
Primary userPolish military aviation
Number built1

TheLWD Żuraw was a Polish utility andliaison aircraft prototype of1951, a high-wing monoplane with single engine, that did not enter production. The name meanscrane.

Design and development

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The aircraft was designed in 1949 by the LWD (Lotnicze Warsztaty Doświadczalne⁣ – Aircraft Experimental Workshops) as a utility and liaison aircraft for thePolish Air Force. The chief designer wasTadeusz Sołtyk. It was the last LWD design. A prototype first flew on 16 May 1951 (pilot Antoni Szymański). Because of a shortage of more powerful engines, it was fitted with the only available license-built Soviet radialShvetsov M-11FR (118 kW, 160 hp). In addition to increased airframe weight (it was 160 kg heavier, than expected), the engine appeared too weak.

To obtainSTOL capabilities, the wings had slats and flaps. The wings were thinner near the canopy to obtain a good view, and they were slightly swept forward. Despite advantages, like short takeoff and landing and low stall speed, the performance was poor and the plane was not ordered for production. It was considered to use more powerful WN-3 orIvchenko AI-14 engines, but the design was abandoned, because Poland had bought a license to produce theYakovlev Yak-12M.

An unusual feature was the triple tail, with two small vertical stabilizers in addition to a main central one. It was meant to improve aircraft stability at high angles of attack.

Usage

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The prototype was painted in Polish Air Force colours and markings, but was not used by the Polish Air Force. In 1951, it was passed to the Aviation Institute (Instytut Lotnictwa) to obtain certification of approval, and next it was used there for a couple of years. In 1952, it was given a civilian registration, SP-GLB. The prototype was withdrawn from use in 1960 and in 1963 given to thePolish Aviation Museum in Kraków, where it remains in a damaged condition.

Specifications

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Data fromJane's All The World's Aircraft 1956–57[1]

General characteristics

  • Crew: 1
  • Capacity: 2
  • Length: 8.26 m (27 ft 1 in)
  • Wingspan: 11.70 m (38 ft 5 in)
  • Width: 4.42 m (14 ft 6 in) (wings folded)
  • Height: 2.56 m (8 ft 5 in)
  • Wing area: 21 m2 (230 sq ft)
  • Aspect ratio: 6.52:1
  • Airfoil: NACA 23012
  • Empty weight: 899 kg (1,982 lb)
  • Gross weight: 1,157 kg (2,551 lb)
  • Powerplant: 1 ×Shvetsov M-11FR air-cooled 5-cylinderradial engine, 120 kW (160 hp)
  • Propellers: 2-bladed wooden, 2.4 m (7 ft 10 in) diameter

Performance

  • Maximum speed: 175 km/h (109 mph, 94 kn)
  • Cruise speed: 140 km/h (87 mph, 76 kn)
  • Range: 950 km (590 mi, 510 nmi)
  • Service ceiling: 2,500 m (8,200 ft)
  • Rate of climb: 2.1 m/s (410 ft/min)

See also

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Aircraft of comparable role, configuration, and era

References

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Wikimedia Commons has media related toLWD Żuraw.
  1. ^Bridgman 1956, p. 193.
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