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Nicholas-Beazley NB-3
The Nicholas-Beazley NB-3, or Barling NB-3, is a two seat, training aircraft of the 1920s.
==Design==
The Barling NB-3 was designed by Walter Barling in 1927. The aircraft was advertised as being able to right itself from any position with hands off the controls and also as being spin-proof. The NB-3 is a low wing tandem-seat, open cockpit aircraft with conventional landing gear. The fuselage was constructed of welded steel tubing with aircraft fabric covering. The wings used a unique double layered corrogated aluminum skin with a smooth exterior that required custom presses to handle the various thicknesses of material along the span. The center section was straight with dihedreal in the outer bays. The spar was also aluminum with a U shaped profile. The aircraft was powered by an Anzani 3 cylinder radial engine, Superior radial or LeBlond 60-5-D.〔(【引用サイトリンク】url=http://www.oldrhinebeck.org/index.php?option=com_k2&view=item&id=135:nicholas-beazley-nb-8g&Itemid=87 )〕 The main gear used long struts attached to the upper fuselage for the largest landing gear geometry. The NB-3 fuselage was widened, giving one cockpit a side-by side seating arrangement to accommodate 3 people. The new aircraft was named the NB-4.
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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