Gull wing

The gull wing was first implemented on a glider, specifically the Weltensegler, which performed its maiden flight in 1921. Its wings, which were externally braced, featured swept-back wingtips with negative incidence relative to the remainder of the main-plane. The Weltensegler also used a unique control system, consisting of a various pulleys and springs connected to a single control stick for the pilot, which warped the wing-tips as directed by the pilot. This unorthodox method relied upon the incidence changing with the increase and release of tension, and was also expected to confer increased stability in pitch and roll by automatic changes in wing-tip incidence; however, it gave no direct control over the wing-tips. Following the Weltensegler's tragic loss, the gull wing was avoided by the majority of aircraft designers for almost a whole decade. During 1930, Alexander Lippisch's record-breaking Fafnir represented a high-profile comeback for the gull wing, which contributed to its resurgence shortly thereafter. Fafnir featured a laterally stabilising dihedral, an uncommon feature for gliders of the era, which spanned roughly 40 percent of the inner wing span. Lippisch had chosen to adopt this configuration for its increased wingtip clearance, as well as the ill-founded belief that it would improve its stability during turns; however, studies have shown that normal gull wing configurations result in significantly less severe and more easily recoverable stalls. Inverted gull wings exhibit the opposite stall behaviour, but both normal and inverted gull wings impede lift-to-drag ratio and climb performance. The performance demonstrated by Fafnir, such as a flight between the Wasserkuppe and Magdeburg in late August 1930 that established a new world record, quickly encouraged numerous aircraft designers to perform their own investigations into the gull wing. Accordingly, numerous other gliders, as well as other platforms, would soon feature broadly similar wing configurations as well. Having become a trend of the glider industry during the 1930s, the gull wing remained a staple feature amongst high-performance sailplanes through to the 1950s. ;Notable gull wing sailplanes: • Bowlus Senior Albatross • DFS Habicht • DFS Kranich • DFS Reiher • Göppingen Gö 3 Minimoa • Lawrence Tech IV "Yankee Doodle" • Lippisch Fafnir • Ross RS-1 Zanonia • Schweyer Rhönsperber • Slingsby Kite • Weltensegler • Ikarus Košava ==Seaplanes==

seaplane with gull wing profile The gull wing design found its way into seaplanes by the early 1930s. As engine power increased, so did the need for large propellers that could effectively convert power to thrust. The gull wing allowed designers to ensure adequate propeller tip clearance over the water by placing the engines on the highest point of the wing. The alternative was placing the engine on a pylon. The first flying boat to utilize the gull wing configuration may have been the Short Knuckleduster, which first flew in 1933. The Dornier Do 26, a high-speed airliner and transport platform, of which six aircraft were built, made its first flight during 1938. The configuration was also used on the US Navy's PBM Mariner and P5M Marlin maritime patrol aircraft. The emergence of long range, land-based jets in the 1950s and the subsequent demise of the seaplane prevented widespread use of the gull wing, although it was still used in some post-war designs, like Beriev Be-12 Chaika (the name means 'gull' in Russian). Examples: • Beriev Be-6 • Dornier Do 26 • Martin P5M Marlin • Piaggio P.136 • Short Knuckleduster ==Landplanes==

c, showing an idea of original Puławski's wing During the late 1920s, the gull wing design found its way into landplanes. In 1928, the Polish aircraft designer Zygmunt Puławski developed the PZL P.1, an experimental fighter aircraft; a major innovation of the PZL P.1 was its relatively high-mounted gull wing. Seeking to protect his new wing arrangement, Puławski filed for an associated patent for this wing arrangement during the following year. The arrangement devised by Puławski has been referred to as the "Puławski Wing" or the "Polish Wing". The PZL P.1 led to a production model, the PZL P.7, of which 149 were produced between 1932 and 1933. The gull wing was used to improve visibility in a high wing arrangement, because such wing could be thinnest by the fuselage, and in theory should limit pilot's view no more than A-pillars of a windscreen in a car body. It was used on multiple fighter aircraft, including the PZL P.11 and Soviet Polikarpov I-15. The PZL P.11 was a further improvement of the PZL P.7 that was in production throughout the early 1930s. It possessed various cutting-edge features for the era in addition to the high-mounted gull wing, such as its all-metal structure and its metal exterior; according to aviation author Jerzy Cynk, the P.11 was commonly considered to have been the most advanced fighter aircraft of its kind in the world upon its introduction. A modern aircraft with a gull wing design is the electric utility aircraft Alia CX300 built by Beta Technologies. Examples: • PZL P.1 • PZL P.6 • PZL P.7 • PZL P.8 • PZL P.11 • PZL P.24 • Henschel Hs 121 • Loire 46 • Polikarpov I-153 • Alia CX300 ==Inverted gull wing==

German ground-attack aircraft of WWII landing on USS Bunker Hill carrying torpedo. During the 1930s, a derivative of the standard design, known as the inverted gull wing, was developed. It was chiefly used on single engine military aircraft with increasingly powerful engines. Before contra-rotating propellers came into use, such powers required larger diameter propellers but clearance between the propeller tip and ground had to be maintained. Long landing gear legs are heavy, bulky, and weaker than their shorter counterparts. The Vought F4U Corsair, designed from the onset as a carrier-based fighter, not only had the largest propeller of any U.S. fighter, but was also expected to face rough landings aboard a pitching carrier deck. By adopting the inverted gull wing, the landing gear could be shorter and allowed to retract straight back (while twisting through 90º to place the mainwheels atop the lower gear strut ends), the latter factor improving internal wing space. The anhedral of the wing's center-section also permitted the wing and fuselage to meet at the optimum angle for minimizing drag, without using wing root fairings or other measures. These wings, which comprised conventional Junkers double-wing construction, reportedly gave the Ju 87 a considerable advantage over its contemporaries during take-off; relatively large lift forces were created through the aerofoil even when flown at a shallow angle, reducing take-off and landing runs. They also provided a high level of ground visibility to the pilot, as well as enabling the use of a shorter undercarriage. Examples: • Aichi B7A • Blohm & Voss Ha 137 • Junkers Ju 87 Stuka • Vought F4U Corsair • Mitsubishi A5M first prototype • Yermolayev Yer-2 ==References==