Английская Википедия:Dewoitine D.513

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The Dewoitine D.513 was a 1930s prototype French monoplane fighter designed and built by Dewoitine.

Development

The D.513 was a single-seat low-wing cantilever monoplane fighter that first flew on 6 January 1936.[1] The D.513 was powered by an 860 hp (641 kW) Hispano-Suiza 12Ycrs1 V-12 piston engine and had a retractable tailwheel landing gear.[1] Testing proved that the D.513 was unstable and not able to reach the expected speeds and it was rebuilt with a new fuselage and a modified tail unit.[1] The changes did not improve the stability or the maximum speed and problems were also found in the engine cooling and landing gear, and further development was halted.[1] The second prototype was modified with landing gear and a radiator from the D.503. It was redesignated the D.514LP and was used in high-speed parachute trials.[1]

Variants

D.513
Prototype with an 860 hp (641kW) Hispano-Suiza 12Ycrs1 V-12 piston engine.[1]
D.514
Originally intended as the second D.513, it was modified for trials including the fitting of a Hispano-Suiza 12Ydrs2 V-12 engine.[1]

Operators

Шаблон:FRA

Specifications (D.513 revised)

Шаблон:Aircraft specs

Шаблон:Aircontent

References

Шаблон:Reflist

Bibliography

Шаблон:Commons category

Шаблон:Dewoitine aircraft

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