Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Byung-Hyuk Kang"'
Publikováno v:
Actuators, Vol 13, Iss 4, p 155 (2024)
This study explores the significance of active suspension systems for vehicles with lower chassis compared to conventional ones, aiming at the development of future automobiles. Conventional linear MR (magnetorheological) dampers were found inadequat
Externí odkaz:
https://doaj.org/article/dc41ca3ca40b4dc49fcc8cda2392c769
Publikováno v:
Actuators, Vol 12, Iss 7, p 287 (2023)
In this study, our focus is on the drop test simulation of an MR (Magnetorheological) damper-based main landing gear (MRMLG), aiming to explore multi-degree-of-freedom (DOF) dynamic models during aircraft landing. Three different 6-DOF dynamic models
Externí odkaz:
https://doaj.org/article/f9d6c47c0e4e4ff5b5deb62373760e56
Publikováno v:
Applied Sciences, Vol 11, Iss 17, p 7895 (2021)
This work presents a novel design model of a magnetorheological (MR) fluid-based shock absorber (MR shock absorber in short) that can be applied to an aircraft landing gear system. When an external force acts on an MR shock absorber, pressure loss oc
Externí odkaz:
https://doaj.org/article/0ebc36512d3748cf824df2e8a3c2b214
In this study, the focus is on the drop test simulation of an MR (Magnetorheological) damper-based main landing gear (MRMLG), aiming to explore multi-degree-of-freedom (DOF) dynamic models during aircraft landing. Three different 6-DOF dynamic models
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3dc21445093b25b36a105642bd6e7ba1
https://doi.org/10.20944/preprints202305.1795.v1
https://doi.org/10.20944/preprints202305.1795.v1
Modeling and Performance Analysis of Linear Part Feeder System Actuated by Piezoelectric Transducers
Publikováno v:
International Journal of Precision Engineering and Manufacturing. 23:57-65
Publikováno v:
Journal of Intelligent Material Systems and Structures. 32:1290-1302
This work presents landing efficiency control of a six-degree-of-freedom aircraft model, which has a controllable landing gear system with magnetorheological damper. Due to lengthy contents, this work is divided into two parts. In Part 1, both the ki
Publikováno v:
Journal of Intelligent Material Systems and Structures. 32:1303-1315
In Part 1 of this work, both the kinematic and dynamic equations of aircraft landing model integrated with magneto-rheological damper were derived. In Part 2, the landing efficiency is analyzed through landing motion simulation which is performed on
Publikováno v:
Journal of Intelligent Material Systems and Structures. :1045389X2211476
This work presents a magnetorheological (MR) damper applicable to the landing gear system in the aircraft. The proposed MR landing gear (MRLG) is modeled as a two degrees of freedom (2-DOF) system for the drop performance evaluation. A mathematical m
Publikováno v:
Applied Sciences; Volume 11; Issue 17; Pages: 7895
Applied Sciences, Vol 11, Iss 7895, p 7895 (2021)
Applied Sciences, Vol 11, Iss 7895, p 7895 (2021)
This work presents a novel design model of a magnetorheological (MR) fluid-based shock absorber (MR shock absorber in short) that can be applied to an aircraft landing gear system. When an external force acts on an MR shock absorber, pressure loss oc
Publikováno v:
Journal of Aircraft. 56:1980-1986
In this research, a two-core type of a semi-active magnetorheological (MR) damper is designed for an airplane landing gear system, and its landing efficiency is evaluated using two different contro...