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Bikle T-6
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Bikle T-6 : ウィキペディア英語版
Bikle T-6

The Bikle T-6 is an American, mid-wing, single seat, glider designed by Paul Bikle and based upon the design of the Schreder HP-14. Even though only one T-6 was built it is noted as the most tested and studied glider with complete data published. It has been used extensively as a comparative reference glider for evaluating other designs during in-flight comparisons.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 37. Soaring Society of America November 1983. USPS 499-920〕
==Design and development==

Bikle developed the all-metal T-6 during the time when he was director of the US National Aeronautics and Space Administration Dryden Flight Research Facility. He changed the design from the HP-14 by adding in to each wing, bringing the span to . The flaps were shortened by each and the ailerons increased in span by a corresponding amount.The airfoil was altered from the stock Wortmann FX 61-163 to simplify construction, even at the cost of some measure of performance. The construction of the airframe was modified to eliminate the use of pop rivets and the structure and assembly requirements were simplified. The flap and flight control systems were also redesigned. Bikle also developed the T-tail, installing it in place of the HP-14's V-tail.〔〔
The T-6 is named for Bikle's competition number "6" and the T-tailed design of the aircraft.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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