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Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds

机译：确定不平衡后缘控制的理论分析，由于超音速下的偏转而具有最小铰链力矩

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Goin, Kennith L;
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年度 1952
页码 1-54
总页数 54
原文格式 PDF
正文语种 eng
中图分类工业技术;
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4. A SIMPLE AND ACCURATE METHOD FOR DETERMINING LARGE DEFLECTIONS IN COMPLAINT MECHANISMS SUBJECTED TO END FORCES AND MOMENTS [C] . A. Saxena Steven, N. Kramer ASME Design Engineering Technical Conferences . 1998

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7. Evaluation of the Control Strategy Performance for Isolated Variable-Speed Wind Turbine Using Different Wind Speed Models at Different Load Cases under Balanced/Unbalanced Excitation [O] . Saber Saleh, Asmaa Farag 2019

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8. THEORETICAL ANALYSES TO DETERMINE UNBALANCED TRAILING-EDGE CONTROLS HAVING MINIMUM HINGE MOMENTS DUE TO DEFLECTION AT SUPERSONIC SPEEDS [R] . Kennith L. Goin 1955

机译：理论分析确定由于超音速的变化而具有最小铰链的不平衡拖尾控制

Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds

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