Girish Mahajan (Editor)

Slingsby Petrel

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Wingspan
  
17 m

First flight
  
December 1938

Length
  
7.25 m

Manufacturer
  
Slingsby Aviation

Slingsby Petrel SSUK Slingsby Petrel

Oldgliders slingsby petrel t13 1 3 5


The Slingsby T.13 Petrel was a British single-seat competition glider built by Slingsby Sailplanes just before World War II.

Contents

Slingsby Petrel Modellers Steve Fraquet Slingsby Petrel

Development

Slingsby Petrel Slingsby T13 Petrel Untitled Aviation Photo 2210050

The Slingsby Petrel was a development of the German DFS Rhonadler designed by Hans Jacobs. It was a single-seat high-performance sailplane with a span of a little under 18 metres, built of wood with a mixture of plywood and fabric covering. It had high cantilever gull wings, though the inner section dihedral was modest. They carried straight taper to fine and rounded tips and ailerons that extended over more than half the span. There were neither flaps nor airbrakes.

Slingsby Petrel Slingsby Petrel by james147741 on DeviantArt

The fuselage had its maximum diameter near the nose, where the long, multipiece canopy blended in smoothly, ending at the wing leading edge. Behind the wings the fuselage tapered and became slender at the tail. The fin and the tailpane were both small in area; the rudder was large, aerodynamically balanced and extended down to the keel. The elevators were tapered, with a cut out for rudder movement. The undercarriage consisted of just a main skid from below the front of the cockpit glazing to mid chord plus a tail bumper.

Operational history

Slingsby Petrel Petrel

The Petrel prototype first flew in December 1938. This aircraft crashed at Camphill, Derbyshire in the British National Championships of July 1939, killing its pilot, the speedway rider Frank Charles. Two more were built and flew for several decades after World War II with clubs in England and Ireland. One of them was a competitor at the 1953 British National Championships, held again at Camphill, by then known as Great Hucklow, after being bowled over in transit by a Rotherham trolley-bus.

Survivors

Slingsby Petrel httpsuploadwikimediaorgwikipediacommonsthu

Only one Petrel, BGA651, the final aircraft, remains airworthy in 2013. It was restored by its owner, Graham Saw. It flies regularly at Vintage Glider Club meetings and has been displayed at Old Warden on Shuttleworth Collection open days.

Slingsby Petrel THE RETURN OF THE PETREL YouTube

Another, BGA418, the second Petrel, is being restored, though not yet on display, at the Western Antique Aeroplane and Automobile Museum (WAAAM) in Hood River, Oregon, United States.

Specifications

Data from Ellison 1971, p. 183 The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde

General characteristics

  • Crew: 1
  • Length: 23 ft 9 in (7.25 m)
  • Wingspan: 56 ft 11 in (17.34 m)
  • Wing area: 180.0 sq ft (16.72 m2)
  • Aspect ratio: 17.9
  • Airfoil: Göttingen 535
  • Empty weight: 440 lb (199.5 kg) equipped
  • Max takeoff weight: 638 lb (289.5 kg)
  • Performance

  • g limits: +6
  • Maximum glide ratio: 27 at 42 mph (67.6 km/h; 36.5 kn)
  • Rate of sink: 106 ft/min (0.54 m/s) minimum, at 35 mph (56.3 km/h; 30.4 kn)
  • Wing loading: 3.6 lb/sq ft (17.5 kg/m2)
  • References

    Slingsby Petrel Wikipedia