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The Beatty-Johl BJ-2 Assegai was a single seat, high performance competition glider built in South Africa in the early 1960s. Only one was built; it was optimised for South African conditions and performed well there, winning two nationals and setting several records, but was less successful under European conditions at the 1965 World Gliding Championships. ==Design and development== The BJ-2 was a successor to the BJ-1, a 60 ft (18.3 m) span glider on which design began in South Africa in 1945 but abandoned before completion as it became clear that the new laminar flow airfoil sections offered better performance. The BJ-2 used one of the 65 series airfoils in conjunction with Fowler flaps. Its design, led by W.A.T. Johl, concentrated on high cross country glide speeds, achieved via a high wing loading and low camber, important in South African gliding conditions with strong thermals and long flights between them. Design work started in 1955 but the BJ-2 was not flown until January 1961, piloted and chiefly built by P.J.Beatty. The BJ-2 was an almost entirely wooden aircraft, both internally and with a plywood skin on all surfaces. The single spar, 50 ft (15.24 m) span, shoulder mounted wings had three pieces, the centre one with a span of 30 ft 1 in (9.17 m), rectangular in plan, the NACA 65 wing section and no dihedral. The outer pieces were trapezoidal and had 5° dihedral, changing to a non-laminar section at the tip, with the ailerons filling all their trailing edge. The centre panel trailing edge was filled with Fowler flaps, which at maximum, 30° extension increased both the camber and the wing area, the latter by 19.5%, for low speed flight in thermals. Small wing tip bodies were added later.〔〔 Its fuselage was a semi-monocoque structure, elliptical in cross-section and tapering uniformly towards the tail. The fin and rudder together were trapezoidal, with a T tail and elevator of constant chord within tapered tips. Lacking the more usual wing mounted airbrakes, the BJ-2 had a pair of petal type, fuselage mounted brakes for glide angle control just aft of the wing. It also had two cruciform braking parachutes deployable from the lower rear fuselage below the rudder. Forward of the wing the upper fuselage line blended smoothly into that of the single piece, sideways opening canopy to limit dive speeds. The undercarriage combined a retractable monowheel, fitted with a brake, and a co-retracting forward skid. The nose was of glass reinforced plastic.〔〔 Camber changing Fowler flaps had been used before on gliders, notably on the 1938 Akaflieg Hannover AFH-4 and the 1948 Cijan-Obad Orao II, though not fitted to this design's later version. Whilst they provided the increased camber needed for low speed climbs, they also increased drag, both by reducing the aspect ratio, raising the induced drag, and by the creation of extra vortexes at the outer ends of the flaps. This penalty was less costly in typically strong South African thermals than in the weaker ones found in northern Europe.〔 The BJ-2 proved to have the intended high speed performance, demonstrated in a series of closed circuit and out and back flights. The fuselage mounted airbrakes proved rather ineffective.〔 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Beatty-Johl BJ-2 Assegai」の詳細全文を読む スポンサード リンク
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