Stress distribution in structural composite lumber under torsion

被引:0
|
作者
Gupta, R [1 ]
Siller, TS [1 ]
机构
[1] Oregon State Univ, Dept Wood Sci & Engn, Corvallis, OR 97331 USA
关键词
D O I
暂无
中图分类号
S7 [林业];
学科分类号
0829 ; 0907 ;
摘要
Stress distribution in fall-size, structural composite lumber (SCL) under torsion was analyzed using finite element analysis (FEA). The objective was to determine shear strength of SCL using orthotropic torsion theory and compare the results to experimental results. The commercial finite element program ANSYS was used to perform the analysis using orthotropic material properties. A three-dimensional, eight-node brick element was used to model the specimens. The FEA showed that SCL is more orthotropic in material behavior than solid-sawn lumber and orthotropic torsion theory should be used to determine the shear strength of SCL. The degree of orthotropicity depends upon two shear moduli in longitudinal-tangential and longitudinal-radial planes. The shear strength based on orthotropic FEA was within 2 percent of experimental results.
引用
收藏
页码:51 / 56
页数:6
相关论文
共 50 条
  • [21] Simulation based modeling of the elastic properties of structural composite lumber
    Bejo, L
    Lang, EM
    WOOD AND FIBER SCIENCE, 2004, 36 (03): : 395 - 410
  • [22] Stress distribution in damaged composite laminates under transverse impact
    Jiang, D
    Shu, DW
    COMPOSITE STRUCTURES, 2004, 63 (3-4) : 407 - 415
  • [24] The effects of circumferential voids or debonds on stress distribution in tubular adhesive joints under torsion
    Shishesaz, Mohammad
    Tehrani, Siavash
    JOURNAL OF ADHESION, 2020, 96 (16): : 1396 - 1430
  • [25] The effects of circumferential voids or debonds on stress distribution in tubular adhesive joints under torsion
    Shishesaz, Mohammad
    Tehrani, Siavash
    Journal of Adhesion, 2019,
  • [26] Buckling of Rectangular Composite Pipes under Torsion
    Takano, Atsushi
    Mizukami, Ryo
    Kitamura, Ryuta
    APPLIED SCIENCES-BASEL, 2021, 11 (03): : 1 - 12
  • [27] Stability of cylindrical composite shells under torsion
    Semenyuk, NP
    Dushek, YY
    Trach, VM
    INTERNATIONAL APPLIED MECHANICS, 2005, 41 (10) : 1170 - 1176
  • [28] Failure prediction of composite laminates under torsion
    Sen, JK
    Fish, JC
    FRACTURE OF COMPOSITES, 1996, 120- : 285 - 306
  • [29] Stability of Cylindrical Composite Shells under Torsion
    N. P. Semenyuk
    Yu. Ya. Dushek
    V. M. Trach
    International Applied Mechanics, 2005, 41 : 1170 - 1176
  • [30] Failure prediction of composite laminates under torsion
    McDonnell Douglas Helicopter Systems, Mesa, United States
    Key Eng Mat, (285-306):