Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Taeyoung Chun"'
Publikováno v:
Journal of Aircraft. 59:1104-1111
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d57ee08fa329fc5d4bb1433a415d72b9
https://doi.org/10.2514/1.c036786
https://doi.org/10.2514/1.c036786
Publikováno v:
Journal of Composite Materials. 56:1753-1764
The conventional representative volume element approach may not be accurate enough in examining stress distribution near singularity in a composite. However, enormous number of degrees of freedom (DOFs) is usually required to discretize the subcompon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07191e93969356fe92f7f845dcb5d9b9
https://doi.org/10.1177/00219983221074511
https://doi.org/10.1177/00219983221074511
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 48:671-680
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::645d410d26ca8960acb6c3b8771e8b0c
https://doi.org/10.5139/jksas.2020.48.9.671
https://doi.org/10.5139/jksas.2020.48.9.671
Publikováno v:
International Journal of Aeronautical and Space Sciences. 16:177-189
This paper presents an all-direct domain decomposition approach for large-scale structural analysis. The proposed approach achieves computational robustness and efficiency by enforcing the compatibility of the displacement field across the subdomain
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cdc7f23fd817541dd6831b8cbe82c715
https://doi.org/10.5139/ijass.2015.16.2.177
https://doi.org/10.5139/ijass.2015.16.2.177
Publikováno v:
Journal of the Korea Society for Industrial and Applied Mathematics. 18:17-26
This paper presents development of an improved domain decomposition method for large scale structural problem that aims to provide high computational efficiency. In the previous researches, we developed the domain decomposition algorithm based on aug
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2fe4f54eb2cd10c7784a905a08fcb73
https://doi.org/10.12941/jksiam.2014.18.017
https://doi.org/10.12941/jksiam.2014.18.017
Publikováno v:
Computational Mechanics. 53:147-158
Finite element based formulations for flexible multibody systems are becoming increasingly popular and as the complexity of the configurations to be treated increases, so does the computational cost. It seems natural to investigate the applicability
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e81ed84dbf50561944a8c6db99ea55a
https://doi.org/10.1007/s00466-013-0898-8
https://doi.org/10.1007/s00466-013-0898-8
Publikováno v:
Journal of Aircraft. 50:539-550
This paper presents an improved structural analysis for a bearingless helicopter rotor. The bearingless rotor usually features a significantly large elastic twist in the flexbeam and additional unique structural characteristics. Thus, it will require
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e841e99b1a0d8a8cefaf1b964855fc5
https://doi.org/10.2514/1.c031920
https://doi.org/10.2514/1.c031920
Publikováno v:
52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
This paper describes application of an improved computational approach based on domain decomposition technique for a large scale structural analysis. We compared computational algorithms corresponding to the original and an improved FETI approach. In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5744cae245f8cb962c06abf3b1816d5
https://doi.org/10.2514/6.2011-1810
https://doi.org/10.2514/6.2011-1810
Autor:
TaeYoung Chun1, Hanyeol Ryu2, Hae Cho Seong2, SangJoon Shin2, Kee, YoungJung3, Kim, Deog-Kwan3
Publikováno v:
Journal of Aircraft. Mar/Apr2013, Vol. 50 Issue 2, p539-550. 12p.
Publikováno v:
International Journal of Naval Architecture and Ocean Engineering, Vol 5, Iss 2, Pp 199-209 (2013)
This paper presents the model test results of 3 new spar platforms which were developed based on the OC3-Hywind spar to support a 5-MW wind turbine. By changing the shape but keeping both volume and mass of OC3-Hywind spar platform, those platforms w
Externí odkaz:
https://doaj.org/article/4ab21d9b8fa1464783f4c2454b3ed17d