The Hurel-Dubois Miles HDM.105 was a transport aircraft fitted with very high aspect ratio wings for research purposes, building on research carried out with the Hurel-Dubois HD.10, and a stepping point to the planned production HDM.106 Caravan. The HDM.105/HDM.106 provided the starting point for the design of the

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Design and development

, a French aircraft designer, became a champion of very high aspect ratio wings in a bid to significantly reduce induced drag, similar to the " Davis wing" of the

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, but with much higher aspect ratios. After testing his wing design on the diminutive HD.10, Hurel was ready to progress to a full size transport aircraft, a joint venture between F.G. Miles Ltd. and , fitting a

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with a very high aspect ratio wing and carrying out comparison tests. The HDM.105 utilised the fuselage, tail unit and engines from Miles Aerovan Mk.4 ''G-AOJF'', fitted with a Hurel designed span 20.5:1 aspect ratio wing of NACA laminar flow sections, supported on aerofoil section lifting struts. The wings were fitted with double-slotted flaps actuated by Miles electric actuators from the original Aerovan. Roll control was by differential ailerons and inter-connected upper-surface spoilers. With no room for fuel in the slender wings, fuel tanks were fitted in the vertical undercarriage strut fairings.

Operational history

The HDM.105, with B-class registration ''G-35-3'' (subsequently re-registered G-AHDM), was first flown on 31 March 1957 by I.A. Forbes, but was later damaged beyond repair in a landing accident at Shoreham on 28 June 1958 and dismantled.

Variants

HDM.106 Caravan

Following the successful testing of the HDM.105 the joint company H.D. et M (Aviation) Ltd, was established to exploit derivatives. The HDM.106 Caravan was to have been an all-metal transport aircraft, with span wings, powered by 2x Lycoming GO-480, 2x Lycoming GSO-480B or 2x Turbomeca Astazou I engines, but the HDM.106 did not progress beyond the drawing board with H.D. et M (Aviation) Ltd. The design for the HDM.106 was sold to Shorts who developed it into the very successful

, but with a much reduced, moderately high, aspect ratio of 11:1.

HDM.107 Aerojeep

The H.D.M.107, known as the Aerojeep, was a military version of the HDM.106 to a STOL light transport requirement of the US Army, to be powered by two Lycoming T53 turboprop engines.

HDM.108

An enlarged HDM.106 designed by Hurel-Dubois.

Miles M.111

The Miles M.111 was proposed as a light single-engined transport utilising the outer wings and struts of the HDM.105, powered by a single Turbomeca Astazou turboprop engine.

Specifications (HDM.105)

References

{{Hurel-Dubois aircraft Miles aircraft Hurel-Dubois aircraft