PublisherDOIYearVolumeIssuePageTitleAuthor(s)Link
Journal of the Korea Institute of Military Science and Technology10.9766/kimst.2020.23.6.5332020236533-541Nonlinear Vibration Analyses of Stiffened Composite Panels under Combined Thermal and Random Acoustic LoadsIn-Jun Choi, Hong-Beom Lee, Jae-Sang Park, In-Gul Kimhttp://jkimst.org/upload/pdf/KIMST-2020-23-6-533.pdf, http://jkimst.org/journal/view.php?doi=10.9766/KIMST.2020.23.6.533, http://jkimst.org/upload/pdf/KIMST-2020-23-6-533.pdf
Shock and Vibration10.1155/2018/9751038201820181-11Nonlinear Random Response Analyses of Panels Considering Transverse Shear Deformations under Combined Thermal and Acoustic LoadsYeong-Nam Kim, Jae-Sang Park, Eun-Soo Go, Min-Hyuk Jeon, In-Gul Kimhttp://downloads.hindawi.com/journals/sv/2018/9751038.pdf, http://downloads.hindawi.com/journals/sv/2018/9751038.xml, http://downloads.hindawi.com/journals/sv/2018/9751038.pdf
Computers & Structures10.1016/0045-7949(87)90279-31987274519-539Nonlinear equilibrium of imperfect, locally deformed stringer-stiffened panels under combined in-plane loadsDavid Bushnellhttps://api.elsevier.com/content/article/PII:0045794987902793?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:0045794987902793?httpAccept=text/plain
Applied Sciences10.3390/app100103872020101387Active Vibration Suppression of Stiffened Composite Panels with Piezoelectric Materials under Blast LoadsChang-Yull Lee, Jin-Young Jung, Se-Min Jeonghttps://www.mdpi.com/2076-3417/10/1/387/pdf
International Journal of Aeronautical and Space Sciences10.1007/s42405-019-00242-w2019213707-722Nonlinear Dynamic Responses of Shear-Deformable Composite Panels under Combined Supersonic Aerodynamic, Thermal, and Random Acoustic LoadsHong-Beom Lee, Yeong-Nam Kim, In-Jun Choi, Jae-Sang Park, In-Gul Kimhttp://link.springer.com/content/pdf/10.1007/s42405-019-00242-w.pdf, http://link.springer.com/article/10.1007/s42405-019-00242-w/fulltext.html, http://link.springer.com/content/pdf/10.1007/s42405-019-00242-w.pdf
Composite Structures10.1016/j.compstruct.2014.10.0032015120285-299Semi-analytical buckling analysis of omega stiffened panels under multi-axial loadsRiccardo Vescovini, Chiara Bisagnihttps://api.elsevier.com/content/article/PII:S0263822314005212?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:S0263822314005212?httpAccept=text/plain
Composite Structures10.1016/j.compstruct.2016.11.0652017162164-181An analytical approach: Nonlinear vibration of imperfect stiffened FGM sandwich toroidal shell segments containing fluid under external thermo-mechanical loadsDao Huy Bich, Dinh Gia Ninhhttps://api.elsevier.com/content/article/PII:S0263822316321316?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:S0263822316321316?httpAccept=text/plain
Composite Structures10.1016/j.compstruct.2015.06.03720151311040-1049Vibration and acoustic responses of composite and sandwich panels under thermal environmentXiangyang Li, Kaiping Yuhttps://api.elsevier.com/content/article/PII:S0263822315005012?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:S0263822315005012?httpAccept=text/plain
Computer Methods in Applied Mechanics and Engineering10.1016/0045-7825(93)90041-u19931031-243-114Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regimeDavid Bushnellhttps://api.elsevier.com/content/article/PII:004578259390041U?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:004578259390041U?httpAccept=text/plain
Composite Structures10.1016/j.compstruct.2019.1113102019227111310Nonlinear vibration of imperfect FG-CNTRC cylindrical panels under external pressure in the thermal environmentK. Foroutan, H. Ahmadi, E. Carrerahttps://api.elsevier.com/content/article/PII:S0263822319322962?httpAccept=text/xml, https://api.elsevier.com/content/article/PII:S0263822319322962?httpAccept=text/plain