Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Jeong-Sik Kwon"'
Publikováno v:
Advanced Composite Materials. 27:439-456
A comprehensive procedure for a mechanically fastened composite laminate joint (ASTM D5961 Proc. A, B) is demonstrated from fixture design to analysis of test results. The ASTM tests are applied to evaluate the standard laminate properties and the co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b99d3b2c271e6cac8cd18c405f47c358
https://doi.org/10.1080/09243046.2017.1405607
https://doi.org/10.1080/09243046.2017.1405607
Publikováno v:
International Journal of Aeronautical and Space Sciences. 18:63-69
In this paper, composite laminate pull-through resistance was analyzed using the FEM method and compared with test results. 2D and 3D simplified FEM models, a nonlinear analysis, and a progressive failure analysis utilizing three composite laminate f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::25706470c626393302e004bebdb84955
https://doi.org/10.5139/ijass.2017.18.1.63
https://doi.org/10.5139/ijass.2017.18.1.63
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 45:21-29
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9bf9318f4e85d96510978a22f198b5b
https://doi.org/10.5139/jksas.2017.45.1.21
https://doi.org/10.5139/jksas.2017.45.1.21
Publikováno v:
Journal of Aerospace System Engineering. 10:43-50
School of Aerospace and Mechanical Engineering, Korea University.Abstract : In order to suggest the optimal manufacturing technology of composite wings of solar-powered unmanned aerial vehicles, this study compared forming technologies to reduce wing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfd29335e6d54e119803b780a17ab9fa
https://doi.org/10.20910/jase.2016.10.1.43
https://doi.org/10.20910/jase.2016.10.1.43
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 41:194-200
In this paper, the results of composite laminate mechanical joints test(ASTM D5961) are compared with the theoretical strength calculations and FEM analysis results. To calculate the S.C.F.(stress concentration factor) on joint strength, equations on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d70d1ffc609a92bb190cc4f93a373e81
https://doi.org/10.5139/jksas.2013.41.3.194
https://doi.org/10.5139/jksas.2013.41.3.194