| contributor author | T. Kant | |
| contributor author | J. R. Kommineni | |
| date accessioned | 2017-05-08T21:15:48Z | |
| date available | 2017-05-08T21:15:48Z | |
| date copyright | July 1994 | |
| date issued | 1994 | |
| identifier other | %28asce%290893-1321%281994%297%3A3%28342%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44796 | |
| description abstract | A refined higher order shear deformation theory for linear and geometrically nonlinear behavior of fiber‐reinforced angle‐ply composite and sandwich laminates is established. Laminae material is assumed to be linearly elastic, homogeneous and isotropic/orthotropic. The theory accounts for nonlinear quadratic variation of transverse shear strains through the thickness of the laminate and higher order terms in Green's strain vector in the sense of von Karman. A simple | |
| publisher | American Society of Civil Engineers | |
| title | Nonlinear Analysis of Angle‐Ply Composite and Sandwich Laminates | |
| type | Journal Paper | |
| journal volume | 7 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(1994)7:3(342) | |
| tree | Journal of Aerospace Engineering:;1994:;Volume ( 007 ):;issue: 003 | |
| contenttype | Fulltext | |
