The Zlín Šohaj () series of club gliders began as a post World War II development of the DFS Olympia Meise. A large number were built in the 1940s and '50s. Design and development The Z-25 Šohaj was designed to be a replacement for the pre-war, German Meise. The latter, designed for the glider competitions of the 1940 Olympics that were abandoned because of hostilities, was widely used in post-war Czechoslovakia. The two types had similar appearances and much in common but the Šohaj significantly improved on the older aircraft by using 5-digit series NACA airfoils rather than the old Göttingen 549; the NACA sections provide more lift at low speeds, improving flight in thermals and lower landing and take-off speeds. They also had a lower pitching moment and hence lower tail loads, allowing the structure to be lightened. The Šohaj's wings were mounted around shoulder height on the ovoid cross section fuselage, enabling a smoother aerodynamic junction than on the Meise, which had a high wing on an almond shaped fuselage. The Šohaj is an all wood-framed aircraft, covered in a mixture of plywood and fabric. It has strongly straight tapered wings (taper ratio 0.28) with elliptical tips, built around a single spar. From the spar forward around the leading edge the wing is ply covered, forming a torsion resistant D-box. Behind the spar the wing is fabric covered except near the roots ahead of an internal, diagonal, drag strut. There is no sweep at one quarter chord and the wings are mounted with 3° of dihedral. Fabric covered ailerons fill about half the span, with airbrakes just inboard of them and immediately aft of the spar. On the early Šohaj 1, first flown in 1947, these are of the DFS type like those on the Meise, opening above the wings. These are also fitted to the LG-125 Šohaj 2 (sometimes written as Z-125) but the later VT-425 Šohaj 3 or Super Šohaj of 1955 has parallelogram action, double blade Schempp-Hirth type airbrakes. The Šohaj 3 also had its wingspan extended from to and was fitted with inboard flaps of the Fowler type, alterations which improved the glide angle, reduced the stalling speed and, through the increased wing loading, raised the maximum cross country speed between thermals. The fuselage of the Šohaj is completely ply skinned, tapering to the tail. The single seat cockpit, placed just ahead of the