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Effect of Winglets on a First-Generation Jet Transport Wing VI - Stability Characteristics for a Full-Span Model at Subsonic Speeds

机译：小翼对第一代射流传动翼的影响VI - 亚音速速度下全跨度模型的稳定性特征

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A wind-tunnel investigation was conducted to identify changes in stability and control characteristics of a model of the U.S. Air Force KC-135A due to the addition of winglets. Data were obtained at Mach numbers from 0.30 to 0.82, at angles of attack from approximately -8° to 16°, and at angles of sideslip to approximately ±12°. The data generally indicate that winglets improve stability and control characteristics.

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作者
Stuart G. Flechner;
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年度 1979
页码 1-70
总页数 70
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Winglets - KC-135A - Stability and control;

机译：小翼 - KC-135a - 稳定性和控制;

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3. Effect of winglets induced tip vortex structure on the performance of subsonic wings [J] . Narayan Gautham, John Bibin Aerospace science and technology . 2016,第NOVa期

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7. Numerical Computation of Subsonic Oscillatory Airforce Coefficients for Wing-Winglet Configurations [O] . C.W. Cheung 2007

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8. Effect of Winglets on a First-Generation Jet Transport Wing. 6:Stability Characteristics for a Full-Span Model at Subsonic Speeds. [R] . flechner, s. g. 1979

机译：小翼对第一代喷气式运输机翼的影响。图6：亚音速速度下全跨度模型的稳定性特征。

Effect of Winglets on a First-Generation Jet Transport Wing VI - Stability Characteristics for a Full-Span Model at Subsonic Speeds

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