| contributor author | Jinsong Huang | |
| 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%2864%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44962 | |
| description abstract | By adopting the energy method, a method of calculating the stability of the rotational composite shell is presented that takes into account the influence of nonlinear prebuckling deformations and stresses on the buckling of the shell. The relationships between the prebuckling deformations and strains are calculated by nonlinear Karman equations. The numerical method is used to calculate the energy of the whole system. The nonlinear equation is solved by combining the gradient method and the amended Newton iterative method. A computer program is also developed. Examples are given to demonstrate the accuracy of the method presented in this paper. | |
| publisher | American Society of Civil Engineers | |
| title | Nonlinear Buckling of Composite Shells of Revolution | |
| 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(64) | |
| tree | Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002 | |
| contenttype | Fulltext | |
