Arama Sonuçları Aerospace engineering.SirsiDynix Enterprisehttps://catalog.iyte.edu.tr/client/tr_TR/default_tr/default_tr/qu$003dAerospace$002bengineering.$0026rm$003dTEZ$002bKOLEKSIYONU0$00257C$00257C$00257C1$00257C$00257C$00257C0$00257C$00257C$00257Ctrue$0026te$003dILS$0026ps$003d300?dt=list2025-07-03T13:33:05ZDesign of HiDAM: highly deployable articulated mast for positioning of satellite componentsent://SD_ILS/0/SD_ILS:22805292025-07-03T13:33:05Z2025-07-03T13:33:05Zby Cebeci, Yunus, author.<br/><a href="https://hdl.handle.net/11147/12798">Access to Electronic Versiyon.</a><br/>Format: El Yazması<br/>Topology optimization of non-linear elastic microstructuresent://SD_ILS/0/SD_ILS:23426682025-07-03T13:33:05Z2025-07-03T13:33:05Zby Güven, Murat, author.<br/><a href="https://hdl.handle.net/11147/13904">Access to Electronic Versiyon.</a><br/>Format: El Yazması<br/>Minimum weight design of carbon/epoxy laminated composites for maximum buckling load using simulated annealing algorithment://SD_ILS/0/SD_ILS:4681902025-07-03T13:33:05Z2025-07-03T13:33:05Zby Gülmez, Erkut, author.<br/><a href="http://hdl.handle.net/11147/4229">Access to Electronic Versiyon.</a><br/>Format: El Yazması<br/>Development of aluminum honeycomb cored carbon fiber reinforced polymer composite based sandwich structuresent://SD_ILS/0/SD_ILS:13524272025-07-03T13:33:05Z2025-07-03T13:33:05Zby Okur, Mehmet Ziya, author.<br/><a href="http://hdl.handle.net/11147/5735">Access to Electronic Versiyon.</a><br/>Format: El Yazması<br/>Stacking sequence optimization and modeling of laminated composite plates for free vibrationent://SD_ILS/0/SD_ILS:20238822025-07-03T13:33:05Z2025-07-03T13:33:05Zby Hasanoğlu, Emre Azim, author.<br/><a href="http://hdl.handle.net/11147/6888">Access to Electronic Versiyon.</a><br/>Format: El Yazması<br/>