查詢結果分析
相關文獻
頁籤選單縮合
題名 | Thermal Buckling of Simply Supported Composite Sandwich Plates= |
---|---|
作者 | Kuo, Shih-yao; |
期刊 | Journal of Aeronautics, Astronautics and Aviation. Series A |
出版日期 | 20060600 |
卷期 | 38:2 民95.06 |
頁次 | 頁131-136 |
分類號 | 447.62 |
語文 | eng |
關鍵詞 | Buckling; Composite sandwich plate; Shear effect; Temperature; |
英文摘要 | An analytical solution is derived for the thermal buckling of a rectangular composite sandwich plate with angle-ply symmetric laminate faces and a honeycomb core. The results show that the buckling mode that sandwich plate will buckle into is dependent on the fiber orientation in the faces and the aspect ratio of the plate. For the square sandwich plate with angle-ply laminated faces, the highest critical bucking temperature is obtained with fibers orientated at 45°. For the rectangular [±θ2/core][92b8] sandwich plate with aspect ratio greater than 2, orientating the fibers in the faces to an angle around 63B0 will give the highest critical bucking temperature. |
本系統之摘要資訊系依該期刊論文摘要之資訊為主。