Zobrazeno 1 - 10
of 205
pro vyhledávání: '"SangJoon Shin"'
Autor:
Sang-Lae Lee, SangJoon Shin
Publikováno v:
Energies, Vol 13, Iss 7, p 1639 (2020)
Within the framework of blade aerodynamic design, the maximum aerodynamic efficiency, power production, and minimum thrust force are the targets to obtain. This paper describes an improved optimization framework for blade aerodynamic design under rea
Externí odkaz:
https://doaj.org/article/dc41e904033d4939b2188e25786339e5
Publikováno v:
Computational Mechanics. 71:801-825
Among numerous approaches that have been presented for computational contact analysis, the node-to-segment (NTS) approach is widely adopted in industrial applications, particularly with the penalty method. However, the pure penalty-method-based NTS a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24e4b2e5efec94d7c77b21bf9971b070
https://doi.org/10.1007/s00466-023-02269-z
https://doi.org/10.1007/s00466-023-02269-z
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 50:889-898
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed6c2db2846c43dd71710b9f1e1c633f
https://doi.org/10.5139/jksas.2022.50.12.889
https://doi.org/10.5139/jksas.2022.50.12.889
Publikováno v:
Journal of the Computational Structural Engineering Institute of Korea. 35:249-257
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3772c0878ff4b2773325505bbc54921d
https://doi.org/10.7734/coseik.2022.35.5.249
https://doi.org/10.7734/coseik.2022.35.5.249
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:
International Journal of Aeroacoustics. 21:115-141
The goal of this paper is to examine the computational approaches for predicting both of the overall sound pressure level (OASPL) at a few locations and acceleration power spectral density (APSD) of surrounding thin plates due to the aero-acoustic pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0eaa63c15f22707ddba109c92a69944a
https://doi.org/10.1177/1475472x221093702
https://doi.org/10.1177/1475472x221093702
Publikováno v:
Journal of the American Helicopter Society; Oct2023, Vol. 68 Issue 4, p1-21, 21p
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 50:173-180
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8b6be2054ad8edd71ca3d6553db580d
https://doi.org/10.5139/jksas.2022.50.3.173
https://doi.org/10.5139/jksas.2022.50.3.173
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:
AIAA Journal. 60:1909-1922
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6630739147c0699a40b31e354ee3ed3
https://doi.org/10.2514/1.j060742
https://doi.org/10.2514/1.j060742