The Bristol Type 92, sometimes known as the Laboratory biplane, was an aircraft built by the Bristol Aeroplane Company to address the differences between wind tunnel cowling models and full scale cowling for radial engines and was designed as a scaled-up version of a wind tunnel model aircraft. One was built and flew in the mid-1920s. Development In the development of the Bristol Badger in 1919, Bristol's chief designer Frank Barnwell had noted discrepancies between wind tunnel model tests and full-size aircraft, particularly in the failure to predict the Badger's lateral instability. He had responded by building the Badger X which had standard Badger wings combined with a very simple fuselage, intended to look like a scaled-up wind tunnel model for comparison. The Badger went on to become a testbed for Bristol's Jupiter radial engine in a variety of cowlings. Once again, it was difficult to extrapolate from wind tunnel measurements on cowling aerodynamics and engine cooling to the full scale, so that the cooling behaviour of cowlings that were aerodynamically efficient was hard to predict. Cooling difficulties were experienced with the Badger and later Jupiter-powered Bristol types like the Bullfinch and Ten-seater. Barnwell's response was again to design a full-scale aircraft which had the simplifications of a typical wind tunnel model, to which could be fitted any of several cowlings over the Jupiter engine; the Type 92 was the result. It was a two-bay biplane without stagger or sweep on the equal span, square-tipped wings. These and the tail unit, which was also very rectangular and simple, were fabric-covered steel strip and tube structures. Part of the Type 92's odd appearance came from the wish to minimise wing-fuselage aerodynamic interactions. To achieve this, the vertical gap between the wings was large: at it was 25% of the span. The undercarriage had a wide track and was a single axle arrangement mounted below the ends of the inner interplane struts. The fuselage was also simple, the structural part being a plywood-covered box girder about square from the nose to aft of the second cockpit, where it tapered in plan only to an edge at the tail. Two streamlined pylons joined the wings to the box, above and below, carrying the fuselage at mid gap. For the aerodynamic investigations, the untapered part of the fuselage could be contained in circular fairings of different diameters; originally a range of five sizes was