| contributor author | John D. Pratt | |
| contributor author | Gerard Pardoen | |
| date accessioned | 2017-05-08T21:16:06Z | |
| date available | 2017-05-08T21:16:06Z | |
| date copyright | April 2002 | |
| date issued | 2002 | |
| identifier other | %28asce%290893-1321%282002%2915%3A2%2855%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44961 | |
| description abstract | Nonlinear finite-element models that predict the load-elongation behavior of single- and dual-bolted conical-head bolted lap joints are developed, and the load-elongation predictions are compared with experimental test data. The study is conducted for several panel thicknesses with a 4.8 mm size fastener and 2024-T3 clad aluminum alloy panels. The model load-elongation predictions are in excellent agreement with experimental test data. The results show that (1) dual-bolted lap joint test results underpredict the strength of single-bolted lap joints; and (2) numerical models may reliably predict the load-elongation behavior of mechanically fastened lap joints at a fraction of the cost and time of experimental testing. | |
| publisher | American Society of Civil Engineers | |
| title | Comparative Behavior of Single-Bolted and Dual-Bolted Lap Joints | |
| type | Journal Paper | |
| journal volume | 15 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2002)15:2(55) | |
| tree | Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002 | |
| contenttype | Fulltext | |