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Haufe Buzzer 2
The Haufe Buzzer 2 is an American high-wing, strut-braced single-seat motor glider that was designed and constructed by Walter Haufe.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 121. Soaring Society of America, November 1983. USPS 499-920〕
==Design and development==
After Haufe's earlier Buzzer was deemed less than successful, due to the insufficiently reliable Nelson Aircraft engine, Haufe retired that design and designed a new aircraft, which became the ''Buzzer 2''. Intended to be a cross between a conventional sailplane and a light aircraft the aircraft was built with a wing span and has a 16:1 glide ratio.〔〔
The Buzzer 2 is constructed with a welded steel tube fuselage and a wooden wing, all covered with doped aircraft fabric covering. The relatively low 8:1 aspect ratio wing uses a single spar and is supported by a single lift strut. The wing employs a modified NACA 2412 airfoil. The landing gear is a fixed monowheel and two wing-mounted outrigger wheels that support the wing during taxiing. The engine is a Curtiss snowmobile engine that turns at a maximum rpm of 6000, powering the propeller through an oil-immersed 2:1 chain reduction drive, giving a propeller speed of 3000 rpm.〔〔
Only one Buzzer 2 was constructed.〔〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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