DescriptionZeitschrift für Flugtechnik und Motorluftschiffahrt v.5 1914, p.68 fig.91-93 renault 12cyl.png
English: Renault V-12 engine, front view. While the accompanying text describes the 100 hp Renault V-12 engine from 1912, the bore/stroke ratio in this drawing suggests that this drawing may actually depict the preceding 90 hp Renault V-12 engine, which differed in the smaller bore size, having a bore of 90 mm and a stroke of 140 mm.
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It is an anonymous or pseudonymous work (the identity of the author has never been disclosed) or a collective work[2] and more than 70 years have passed since its publication (CPI art. L123-3);
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