| contributor author | John D. Pratt | |
| contributor author | Gerard Pardoen | |
| date accessioned | 2017-05-08T21:16:05Z | |
| date available | 2017-05-08T21:16:05Z | |
| date copyright | January 2002 | |
| date issued | 2002 | |
| identifier other | %28asce%290893-1321%282002%2915%3A1%2820%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44957 | |
| description abstract | Nonlinear finite-element models are developed that predict the load-elongation behavior of conical-head bolted lap joints, and the load-elongation predictions are compared with experimental test data. The study is conducted for several panel thicknesses with three fastener sizes and three panel materials. The model load-elongation predictions are in excellent agreement with experimental test data. Model parameters, such as part discretization, material model selection, sliding interface friction coefficients, and convergence tolerances, are discussed. A means of inducing clamp in the joint is also developed. The results show that nonlinear finite-element analysis may reliably predict the behavior of conical-head bolted joints. | |
| publisher | American Society of Civil Engineers | |
| title | Numerical Modeling of Bolted Lap Joint Behavior | |
| type | Journal Paper | |
| journal volume | 15 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2002)15:1(20) | |
| tree | Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 001 | |
| contenttype | Fulltext | |