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Akaflieg Berlin B12 : ウィキペディア英語版 | Akaflieg Berlin B12
The Akaflieg Berlin B12 is a high performance two-place glider aircraft that was designed and built in Germany.〔 Conceived as a research vehicle, only one unit was constructed. ==Development== The students at Akaflieg Berlin set out to improve the performance of modern gliders by reducing drag. To improve a modern glider's performance through modifying the aerofoil sections is time consuming and very costly, so to reduce costs the group utilised production wings from a Schemp-Hirth Janus B, shortened to 18.2m (59.71 feet), allowing the students to concentrate their efforts and budget on improving the fuselage.〔 The shape and profiles of the new fuselage were developed at the ''Institut für Luftfahrzeugbau '' (Institute for aircraft industry) and a new two-seat fuselage was constructed using contemporary GFRP (Glass-fibre Re-inforced Plastic) techniques in a monocoque shell.〔
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「Akaflieg Berlin B12」の詳細全文を読む
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