| ANALYSIS OF SHEAR STRESS DISTRIBUTION IN HONEYCOMB AIRCRAFT WING STRUCTURE SUBJECTED TO (S.T.) TORQUE |
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| 摘 要： | ＡＮＡＬＹＳＩＳＯＦＳＨＥＡＲＳＴＲＥＳＳＤＩＳＴＲＩＢＵＴＩＯＮＩＮＨＯＮＥＹＣＯＭＢＡＩＲＣＲＡＦＴＷＩＮＧＳＴＲＵＣＴＵＲＥＳＵＢＪＥＣＴＥＤＴＯ（Ｓ．Ｔ．）ＴＯＲＱＵＥＫｈａｌｉｄＭ．Ｔａｈｉｒ，ＺｈａｎｇＸｉｎｇ（ＤｅｐａｒｔｍｅｎｔｏｆＦ...
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ANALYSIS OF SHEAR STRESS DISTRIBUTION IN HONEYCOMB AIRCRAFT WING STRUCTURE SUBJECTED TO (S.T.) TORQUE |
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| Abstract: | Using the method of elasticity, an analytical approach is developed to analyze the shear stress in a honeycomb wing structure with a large aspect ratio under the condition of free torsion. The formulas of shear stress, warping and angle of twist are derived. These formulas are both useful and convenient from the point of view in the structure design. |
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| Keywords: | honeycomb structures wings shear stress free torsion analytical method |
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