|
The Makhonine Mak-10, was a variable geometry research aircraft, built to investigate variable area / telescopic wings during 1931 in France. ==Design and development== In the early 1930s several designers became interested in the possibility of changing the configuration of wings between take off and fast flight. Two routes were explored, the first primarily involving camber and hence lift coefficient reduction and the other a decrease of wing area by span reduction at high speed. The Schmeidler variable wing and that of the Gloster built Antoni-Breda Ba.15 were examples of the first group and the Makhonine Mak-10〔 of the second. Details of the Mak-10 are sparse but its novel feature was a telescopic wing which increased the span for take-off by or 60% of its high speed configuration. The outer panels retracted into the central ones, their inner ends supported on bearings rolling along one or more spars. The ends of the centre section were reinforced with cuffs. The wing apart, it was a conventional cantilever low wing monoplane, with twin open cockpits, the rear one sometimes faired in, and faired, fixed landing gear.〔 It was powered by a , three bank, W-configuration, twelve cylinder Lorraine 12Eb engine.〔 The first flight of the Mak-10 was on 11 August 1931.〔 During four years of development the Mak-10 was re-engined with a Gnome-Rhône 14K Mistral Major fourteen cylinder, two row radial engine which gave it a top speed of and the new designation Mak-101.〔(【引用サイトリンク】title=Machonine Mak-10 )〕 44 years later, the Akaflieg Stuttgart FS-29 experimental high performance sailplane also used telescopic wings to optimise both low speed thermalling and high speed penetration performance without the added induced drag of camber and area changing flaps. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Makhonine Mak-10」の詳細全文を読む スポンサード リンク
|