Czerwiński CW 7
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| CW 7 | |
|---|---|
 | |
| General information | |
| Type | Aerobatic glider |
| National origin | Poland |
| Manufacturer | ZASPL |
| Designer | Wacław Czerwiński |
| Number built | c.10 |
| History | |
| First flight | 13 December 1934 |
The Czerwiński CW 7 was a Polish aerobatic glider first flown in 1934. Despite a structural weakness that prevented inverted flight, a small batch of CW 7s were used by several aeroclubs until the start of World War II.
In the mid-1930s interest in glider aerobatics was growing in Polish aeroclubs, leading to an official requirement for an aircraft specifically designed for the task. Two gliders resulted, the Sokól from Antoni Kocjan and Wacław Czerwiński's CW 7. The latter, like all but one of his earlier glider designs, was built in the workshops of ZASPL, the Aviation Association of Students of the Lwów Technical University.[1]
The CW 7 was an all-wood aircraft with a high, two-part wing built around twin spars. In plan the wing was rectangular out to long semi-elliptical tips. It was braced with parallel pairs of airfoil-section struts from the lower fuselage to the spars. The upper surfaces were plywood covered to the rear spar across the whole span. Between the fuselage and the struts the lower wing surfaces were also ply covered to the rear spar but beyond the struts only to the forward spar. Elsewhere, top and bottom, the wing was fabric covered.[1][2]
The fuselage was an oval section, ply-covered semi-monocoque with an open cockpit ahead of the wing leading edge. It tapered aft to the empennage which was wire-braced, with fixed surfaces covered with ply and control surfaces which were largely fabric covered apart from ply tips. The CW 7's small fin carried a full, rounded, balanced rudder; its tailplane was mounted near the base of the fin and had split elevators. The glider landed on a pneumatically sprung skid.[1]