The Gwinn Aircar was a single-engined biplane

Biplane

A biplane is a fixed-wing aircraft with two superimposed main wings. The Wright brothers' Wright Flyer used a biplane design, as did most aircraft in the early years of aviation. While a biplane wing structure has a structural advantage, it produces more drag than a similar monoplane wing...

 with a cabin for two, designed in the USA as a safe and simple private aircraft. Lacking a rudder, it had several unusual control features as well as an early tricycle undercarriage. Development was abandoned after a crash in 1938.

Design

The Gwinn Aircar was the only product of the aircraft manufacturing company set up by Joseph M. Gwinn Jr, who also designed it. He had previously worked with Consolidated Aircraft

Consolidated Aircraft

The Consolidated Aircraft Corporation was founded in 1923 by Reuben H. Fleet, the result of the Gallaudet Aircraft Company's liquidation and Fleet's purchase of designs from the Dayton-Wright Company as the subsidiary was being closed by its parent corporation, General Motors. Consolidated became...

. The Aircar was intended as a safe, easy to fly aircraft that would neither stall

Stall (flight)

In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases. This occurs when the critical angle of attack of the foil is exceeded...

 nor spin

Spin (flight)

In aviation, a spin is an aggravated stall resulting in autorotation about the spin axis wherein the aircraft follows a corkscrew downward path. Spins can be entered intentionally or unintentionally, from any flight attitude and from practically any airspeed—all that is required is sufficient yaw...

. It used a simplified control system without a rudder. A fuselage which deepened rapidly behind a small radial engine and ended with a fin integrated into it, together with a tricycle undercarriage with a tall and faired front leg, gave the Aircar an unusual appearance.

The Aircar was a single bay biplane with parallel chord, unswept wings with strong stagger

Stagger (aviation)

In aviation stagger refers to the horizontal positioning of a biplane, triplane, or multiplane's wings in relation to one another.An aircraft is said to have positive stagger, or simply stagger, when the upper wing is positioned forward of the lower wing, such as the de Havilland Tiger Moth or...

. The wings were built around two wooden spars, with metal ribs and edges but fabric covered; they were fixed to the upper and lower fuselage. The interplane struts were N-shaped, linking upper and lower spars, aided by one diagonal strut on each side running from the upper rear spar to the lower forward spar. Full span ailerons were fitted to both upper and lower wings.

The Aircar was initially fitted with a 95 hp (70 kW) Pobjoy Niagara II

Pobjoy Niagara

|-See also:-Bibliography:* Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9...

 engine, a small diameter radial. The driveshaft of the two-bladed propeller was offset above the engine centre by spur reduction gearing. An exhaust pipe led back over the cabin and the upper wing. The cabin windscreen was ahead of the wing leading edge but the glazing extended aft to beyond the trailing edge, pilot and passenger sitting side-by-side under it. Entry was by a pair of forward hinged, car type doors, one on either side. The all-metal, stressed skinned fuselage bulged rapidly behind the engine and was roughly circular in cross section between the wings. Seen from the side the fuselage depth decreased only gently, but in plan it narrowed rapidly, ending in a vertical knife edge. The tailplane, mounted on the centreline, had a curved leading edge and carried elevators. The deflection range of these was limited to an overall 8.5°. The original fin had near straight leading edges both above and below the fuselage, terminating in a vertical, rudderless trailing edge carrying only a trim tab below the centreline.

The tricycle undercarriage, unusual at the time, had short main legs made possible by the combination of lower fuselage depth and hence lower wing position, together with the offset propeller. These legs were joined to the front wing spar close to the fuselage, cross braced and splayed outwards to increase the track. The front leg, mounted just behind the engine was much longer; all three legs were faired and carried wheels enclosed in spats.

Control of the Aircar was also unusual. A column mounted wheel moved the ailerons and fore and aft motion of the column operated the elevators as normal. Turns were made by banking. The trim tab on the fin compensated for propeller torque and was directly linked to the throttle. Instead of a rudder bar, a pedal operated the flaps used for takeoff and landing. The wheel brakes were also foot operated and the nosewheel was steered with the control column wheel. At takeoff the flaps were initially retracted and the aircraft accelerated; at the appropriate speed the flaps were lowered and the Aircar left the ground. With elevators up this "zoom" was rapid but ended in level flight, whilst with them down the zoom was gentler and turned into a steady climb. Landings were made from a low speed approach with flaps extended; throttled back, the Aircar adopted a horizontal attitude, the elevator only controlling the sink rate.

Development

The first flight of the Aircar was in early 1937 and a second was built soon afterwards. Tests led to changes in the engine cowling, to experiments with a four-bladed propeller produced by mounting a pair of two-bladed ones at right angles on the same shaft and also to a serious revision of the fin. Its previously angular leading edge was replaced with a more curved and snub shape above the fuselage, though mostly retaining the vertical trailing edge. The line of lower fuselage was straightened so that the lower part of the fin was integrated into it.

These trials showed that with the 95 hp Niagara II engine the Aircar was underpowered, so the second aircraft was re-engined with the more powerful, but similar diameter, 130 hp (97 kW) Niagara V.

A sales tour followed: by 1938 the well known pilot Frank Hawks

Frank Hawks

Frank Monroe Hawks served in the U.S. Army in World War I and was known during the 1920s and 1930s as a record breaking aviator, using a series of Texaco-sponsored aircraft, setting 214 point-to-point records in the United States and Europe...

 had been appointed Vice-President and Sales Manager of Gwinn Aircar Company Inc. and he and Nancy Love (née Harkness) flew the Aircar at a variety of meetings including the US national Air Races at Cleveland in September 1937. Here it was reported as handling well both in the air and on the ground. In August 1938 Hawks and his passenger died on colliding with power cables shortly after takeoff. The surviving Aircar was donated to Consolidated Aircraft, Gwinn's old employers, and development ceased.

Specifications (Niagara II engine)

External Links

• "Safety Plane For Amateurs Runs Like A Car" Popular Science Monthly, November 1937