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Schreder HP-17 : ウィキペディア英語版 | Schreder HP-17
The Schreder HP-17 was an American mid-wing, V tailed, single seat, experimental glider designed by Richard Schreder to test a new airfoil section.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 23. Soaring Society of America, November 1983. USPS 499-920〕 ==Design and development== The HP-17 was designed to test a new airfoil section, the Wortmann FX 72 MS-150A. This airfoil is a high-lift, low drag section that Scheder thought would be a good sailplane design.〔 The HP-17 is all-metal in construction, except for its foam wing ribs. The wing features water ballast carried inside the wing spar. The wing also has full-span flaps and spoilerons in place of ailerons.〔
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「Schreder HP-17」の詳細全文を読む
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