To eliminate these shortcomings, the English designer D. Miles in the year 1940 developed the design of a deck fighter with a "tandem" scheme. The front wing area was 60 percent rear area. The use of this arrangement made it possible to reduce the size of the wings, that is, they could be made not folding, but the flaps deflected simultaneously down on both bearing surfaces should have provided low landing speed.
To test this idea at the aviation firm Phillips & Powis Aircraft Limited, under the direction of Miles, built an experimental aircraft M.35. George Miles wanted to name the plane Dragonfly, which was the name used for the de Havilland DH.90 and the project was given the name Libellula. The layout of the M.35 was conceived as suitable for a carrier-based fighter; the pilot was positioned as far ahead as possible, and the engine and pusher propeller were installed behind the rear wing. Since the lift was provided by two wings, the span of which could be reduced, there was no need to fold them.
The M.35 fighter was a single-seat all-wood monoplane equipped with a pushing propeller. The front bearing surface served to accommodate the elevators, the rear - ailerons. In addition, both surfaces were equipped with landing flaps. Vertical plumage - washers at the end of the wing. The plane had one interesting feature - a significant sweep of the main wing tips. Swept wing improves road stability. In addition to the three-wheeled chassis with a nose wheel, there was an additional wheel at the back, which prevented the propeller from crashing when landing with a significant angle of attack.
The M.35 aircraft was manufactured and lifted into the air six weeks after the start of construction. The first prototype, under registration number U-0235, took off on May 1 of the year 1942. In reality, this machine was not a real fighter, but rather demonstrated the technology, it was not even equipped with weapons.
During the tests, it turned out that the aircraft had a significant longitudinal instability. Tests in a wind tunnel showed that this problem can be eliminated. The stability of the aircraft was improved by changing the centering. Despite the challenges identified during the tests, Miles proposed this project to the Admiralty of Great Britain. However, taking into account all the identified shortcomings, as well as taking into account that the fighters that were in service with the British Navy exceeded the M. 35 in all respects, the production contract was not signed.
In addition to the M.35 Libellula, George Miles developed the M.XNXX heavy bomber in the same way. The new car had to be equipped with three turbojet engines or, for a start, two high-altitude Rolls-Royce Merlin 39 (Rolls-Royce Merlin) or Bristol Hercules VIII (Bristol Hercules). Under the designation of M. 60B, a bomber model was built on the 39 / 5 scale of its actual size. 8 July 22, the unit took off and showed good aerodynamic stability. Initially, flight tests were carried out privately, but in 1943, the aircraft was transferred to Farnborough at the Royal Aviation Research Institute, where the tests were stopped after two accidents.
Aircraft performance characteristics:
Length - 6,20 m;
Height - 2,06 m;
The span of the upper wing - 6,10 m;
The span of the lower wing - 6,22 m;
Wing area - 12,50 m2;
Empty weight - 660 kg;
Normal take-off weight - 839 kg;
Engine type - piston engine de Havilland Gipsy Major;
Power - HP 130;
Cruising speed - 224 km / h;
Maximum speed - 358 km / h;
Practical range - 320 km
Practical ceiling - 6200 m;
Armament - not installed;
Crew - 1 man
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