@article{oai:muroran-it.repo.nii.ac.jp:00010579,
 author = {NISHIZAWA, Tadashi and SAKAMOTO, Hiraku and 坂本, 啓 and OKUMA, Masaaki and FURUYA, Hiroshi and SATO, Yasutaka and OKUIZUMI, Nobukatsu and 奥泉, 信克 and SHIRASAWA, Yoji and MORI, Osamu},
 issue = {ists29},
 journal = {TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN},
 month = {},
 note = {application/pdf, This study estimates the effect of creases, or plastic wrinkle lines, on the out-of-plane stiffness of solar sails. A method to simulate the crease effects using reduced-order finite-element (FE) models is proposed, and is applied to a practical solar sail architecture. A detailed crease shape is determined by a geometrically nonlinear FE analysis using a simple model first; the effect of creases is then replaced by beam elements. This method substantially reduces the computational effort required for the FE analysis of a solar sail model. The result suggests the significant impact of creases on membrane's out-of-plane stiffness when the tension level in the membrane is small.},
 pages = {Pc_107--Pc_113},
 title = {Evaluation of Crease Effects on Out-of-plane Stiffness of Solar Sails},
 volume = {12},
 year = {2014},
 yomi = {サカモト, ヒラク and オクイズミ, ノブカツ}
}