Bernard SIMB V.1
French airplane

The Bernard SIMB V.1 was a French single seat racing monoplane designed to compete for the 1924 Beaumont Cup. It crashed on its first flight and was not rebuilt.
Design and development
The Bernard V.1 is alternatively known as the SIMB V.1: the Société Industrielle des Métaux et du Bois (SIMB) was the second of several aircraft companies founded successively by Adolphe Bernard. The V.1 was a single-engine, single-seat monoplane designed to compete for the Beaumont Cup, a French competition held in 1924 requiring a 300 km (186 mi) flight round a 50 km (31 mi) circuit at Istres at an average speed of over 290 km/h (180 mph).
The V.1 had a cantilever shoulder wing of thin section, built around four spars with plywood and fabric covering. Straight edged beyond the centre section, it tapered only slightly to the oblique tips. The tailplane had curved, swept leading edges and carried split elevators with a cut-out for rudder movement. The fin was almost triangular, with a slightly convex leading edge; it carried a pointed rudder on a vertical hinge extending to the bottom of the fuselage.
The smooth, oval section fuselage was ply and fabric covered, tapering towards the tail. The pilot sat low down in a small open cockpit with narrow streamlined dorsal fairings in front and behind.
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This entry incorporates text from “Bernard SIMB V.1” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.