WING LEADING EDGE – INVESTIGATION OF RAIN DAMAGE ON -

机译：WING LEaDING EDGE - 对雨水损害的调查 -

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A. To determine the effect of an outer skin bond separation on the static strength of a 4W5298-1 wing leading edge section.nB. To duplicate with high velocity air and waterna specified type of outer skin bond separation.nC. To determine the effectiveness of a thin neoprene coating on the edge of a wing leading edge as a protection from rain damage.

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年度 1964
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
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3. SEPARATION　CONTROL　FOR　THE　OUTWING　OF　A　STRAKE－WING　BY　ROTATING　CONE　PLACED　NEAR　THE　LEADING　EDGE [J] . 中国航空学报：英文版 . 1996,第002期
4. Aerodynamic load control on a dynamically pitching wind turbine airfoil using leading-edge protuberance method [J] . Y. N. Zhang, M. M. Zhang, C. Cai, 力学学报：英文版 . 2020,第002期
5. Modelling bird impacts on an aircraft wing - Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics [J] . M A McCarthy, J R Xiao, N Petrinic, International journal of crashworthiness . 2005,第1期

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7. Computational fluid dynamics investigation of finding appropriate location of fluidic anti-icing protective panel on leading edge of wing [J] . Afghari Mohammad Reza, Vaziry Mohammad Ali, Mostofizadeh Ali Reza Proceedings of the Institution of Mechanical Engineers . 2019,第2期

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WING LEADING EDGE – INVESTIGATION OF RAIN DAMAGE ON -

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