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Planning for a new fighter built around the new 1250 HP in-line liquid cooled FIAT engine (tendered to the 1938-39 competition for new engines and designated A.38) started immediately. The job was trusted to the II Design Office (Gabrielli) in Turin. First result was a somewhat P-40-like design as far as the fuselage, using a wing with the same plan of the G-50. The A.38 evolved too, and influenced the design of successive version of the fighter project. First image (they are very low resolution, you'll understand... ) in the oldest version known, from July 1939. Back then the A.38 was a conventional V-engine with the compressor on the back and driving a conventional three-blade spinner. In 1940, the engine was redesigned as an inverted V, with the compressor positioned under the main block, thus shortening the power pack. The spinner became two contrarotating two-blade units. This version can be seen in second and third image. The wing remained the G-50 derived one. In fourth image, the final evolution (May 1941) of the A.38-powered G-55. The spinner is back to the three-blade single rotation type, and the wing follows the new planform that will be retained in the DB-powered version. As a comparison, I include in the fifth image a depiction of the CS-38, an alternative projected that was commissioned by FIAT management (they were used to pit one design office against another, they had four of them, two in Aeronautica d'Italia, one in CANSA in Novara and the final one in CMASA in Pisa). Ing. Manlio Stiavelli designed the CS-38 using as a reference the A.38 inverted V engine with the three-blade propellers. I think that this was from circa late 1940, early 1941.
I'll post the CS-38 data in a reply.
I'll post the CS-38 data in a reply.