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Whigham GW-7 : ウィキペディア英語版 | Whigham GW-7
The Whigham GW-7 is an American mid-wing, single-seat, 15 metre class glider that was designed and constructed by Gene Whigham, a retired Convair flight test engineer. ==Design and development== Whigham's last glider design was the GW-7. The aircraft was completed and first flew in 1987.〔〔 The GW-7 is of all metal construction, has a wing span and employs a NASA NLF(1)-0215F airfoil. The flaps and ailerons are interconnected. The flaps travel +/-10° in normal flight in concert with the ailerons and then can be deployed to 60° for glidepath control on landing.〔 Only one GW-7 was constructed and it was registered with the Federal Aviation Administration as an ''Experimental - Amateur-built''.〔
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「Whigham GW-7」の詳細全文を読む
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