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Custer Channel Wing : ウィキペディア英語版 | Custer Channel Wing
The Custer Channel Wing was a series of American-built experimental aircraft designs of the 1940s and 1950s incorporating a ''half-barrel'' shaped section to each wing. ==Initial design== Willard Custer filed a United States patent in 1929 for a wing design incorporating a semi-circular channel or "half barrel" shape in which an engine was to be fitted in pusher mode. Custer claimed that this layout, the channel wing, which gave STOL operating capabilities, resulted in a design "which is an aircraft not an airplane. It does not plane the air to fly, rather it brings the air to the lift surfaces and reduces pressure to fly at 8 to 11 mph"〔(aerofiles.com )〕
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「Custer Channel Wing」の詳細全文を読む
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