Zhou Zhu-lin. Selection of the Optimum Parameters for Sandwich Construction with Honeycomb Core[J]. Applied Mathematics and Mechanics, 1985, 6(6): 541-549.
Citation: Zhou Zhu-lin. Selection of the Optimum Parameters for Sandwich Construction with Honeycomb Core[J]. Applied Mathematics and Mechanics, 1985, 6(6): 541-549.

Selection of the Optimum Parameters for Sandwich Construction with Honeycomb Core

  • Received Date: 1981-01-03
  • Publish Date: 1985-06-15
  • The minimum weight of sandwich construction which is regarded as objective function has been discussed. Under given constraint condition of the strength or the stiffness, the four optimum parameters of sandwich construction with honeycomb core thickness of the face tf. thickness of the honeycomb core hc, thickness of the honeycomb wall ts, side length of the honeycomb cell c, are evaluated. By using constraint condition of the strength, a equation of high degree is finally solved. In the constraint condition of the stiffness, the constraint optimization problem is treated as inconstraint optimization problem with the method of obtaining extreme value solution by undetermined parameter multiplication. Also, the results are discussed.
  • loading
  • [1]
    周祝林,玻璃钢蜂窝夹层结构制造、性能和设计简介,玻璃钢,4 (1980), 26-37.
    [2]
    南京大学,《最优化方法》(1978).
    [3]
    上海玻璃钢研究所,《玻璃钢结构设计》(1980).
    [4]
    上海玻璃钢研究所.玻璃钢蜂窝夹层结构基本性能,玻璃钢,2 (1975), 13-54.
    [5]
    周祝林,蜂窝夹层板的极限强度,力学学报,1 (1983), 62-69.
    [6]
    周祝林,玻璃钢蜂窝夹层柱压缩的极限强度(1979).
    [7]
    中国科学院力学所,夹层板壳的弯曲、稳定和振动(1978).
    [8]
    AD 709656.Weight optimization of structural sandwich panels (1970).
    [9]
    AD 715989.Minimum weight structural sandwich(1970).
    [10]
    Alspaugh.D.W and S.N.Huang.Minimum weight design of axisymmetric sandwich plates.AIAA J.14.12(1976).
    [11]
    Huang.S.N.and D.W.Alspaugh.Minimum weight sandwich beam design. AIAA J.,12(1974).
    [12]
    Stehlin.P,and L.Holsteinson.Minimum weight design of orthotropic sandwich panels loaded in compression and shear. FFA Report 122.
    [13]
    Александров А.Я.и М.П.Наумова,Онтималъные параметры треслойных пластин и пологих оболочек с сотовым заполнителем при сжатии,Расчеmы Злеменmоб Абuачuоных Консmрукчuu,4(1965).
    [14]
    Turvey G.J.,Uniformly loaded simply supported. antisymmetrically laminated. cross and angle-ply strips on a winkler pasternak foundation.Aeronautical Journal(1976).222-226.
    [15]
    Turvey.G.J.,Buckling of simply supported laminated plates on elastic foundations.Aeronautical Journal(1976).530-535.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1829) PDF downloads(602) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return