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Trager-Bierens T-3 Alibi : ウィキペディア英語版 | Trager-Bierens T-3 Alibi
The Trager-Bierens T-3 Alibi is an American high-wing, V-tailed, single seat glider that was designed and constructed by Kempes Trager and John Bierens.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 66, Soaring Society of America November 1983. USPS 499-920〕 ==Design and development== The T-3 project was commenced in 1949, with the aircraft completed in 1951. The design aim was to produce a performance sailplane without having to build one from scratch. To achieve this goal the wings from a Laister-Kauffmann LK-10 were used.〔〔 Using the wood and fabric LK-10 wings, Trager and Bierens built a new-design fuselage from aluminium. The fuselage included a V-tail and a retractable monowheel landing gear. Later the wing was rebuilt to a new design that used the original spar. A new tail was also built at this time. The designers spent a lot of effort getting the wing surface smooth, which paid off later in contest results. The span wing employs a NACA 4418 airfoil at the wing root and a NACA 4409 at the wing tip.〔〔 Only one T-3 was built. Originally registered as N909D, the registration was later changed to N9098. The aircraft is in the Experimental - Amateur-built category.〔〔
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