通过建立复合材料格栅结构单元的基本力学假设和分析模型,推导了一种新的等效刚度计算方法,用于分析复合材料格栅加筋板的总体稳定性.该方法充分考虑了筋条和面板的相互作用和中面偏移效应,并具有通用性.结合Rayleigh-Ritz能量近似法,推导出了求解加筋板总体屈曲载荷的通用特征方程;分析了多种算例,并与修正平铺法进行了比较,结果吻合得很好.
参考文献
[1] | 张志峰,陈浩然,李煊,等.先进复合材料格栅圆柱壳优化设计的混合遗传算法[J].复合材料学报,2005,22(2):166-171.Zhang Zhifeng,Chen Haoran,Li Xuan,et al.Hybrid genetic algorithm for optimum design of advanced grid composite circular cylinders[J].Acta Materiae Compositae Sinica,2005,22(2):166-171. |
[2] | Meink T E,Gregoreck G.Composite grid vs composite sandwich:A comparison based on payload shroud requirements[C]//IEEE Aerospace Conference Proceedings.Manhattan Beach:IEEE Aerospace and Electronics Systems Society,1998,4:215-220. |
[3] | Jaunky N,Knight N F,Ambur D R.Formulation of an improved smeared theory for buckling analysis of grid-stiffened composite panels[J].Composite Part B,1996,27B(5):519-526. |
[4] | Kidane S,Li G Q,Helms J,et al.Buckling load analysis of grid stiffened composite cylinders[J].Composites,2003,34:1-9. |
[5] | Jaunky N,Knight N F,Ambur D R,et al.Buckling of arbitrary quardrilateral anisotropic plates[J].AIAA Journal,1995,33(5):938-944. |
[6] | Jaunky N,Knight N F,Ambur D R,et al.Buckling analysis of general triangular anisotropic plates using polynomials[J].AIAA Journal,1995,33(12):2414-2417. |
[7] | Jaunky N,Knight N F,Ambur D.Optimal design of gridstiffened composite panels using global and local buckling analyses[J].J Aircr,1998,35(3):478-486. |
[8] | Collier C,Yarrington P.Composite grid-stiffened panel design for post buckling using hypersizer,AIAA-2002-1222[R].Denver Colorado,2002:1-9. |
[9] | Wang J T S,Hsu T M.Discrete analysis of stiffened composite cylindrical shells[J].AIAA J,1985,23(3):1753-1761. |
[10] | Gendron G,Gurdal Z.Optimal design of geodesically stiffened composite cylindrical shells,AIAA Paper No.92-2306-CP[R].1992:2431-2441. |
[11] | Troitsky M.Stiffened plates:Bending,stability and vibration[M].Amsterdam:Elsevier Science Publishing Company,1976:36-120. |
[12] | Reddy A D,Valisetty Rao R,Rehfield L W.Continuous filament wound composites concepts for aircraft fuselage structures[J].AIAA Journal of Aircraft,1985,22(3):249-255. |
[13] | Phillips J L,Gural Z.Structural analysis and optimum design geodesically stiffened composite panels,NASA CCMS-90-50(VPI-E-90-08),Grant NAG-1-643[R].1990:1-268. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%