Whirl Tower Test for Examining the Influence of Dissimilar Helicopter Rotor Blades on the Hub Loads
연구자
Lee, C.B., Kong, K.H., Ryi, J., Im, B., Kang, S.-H., Hwang, M.H., Jo, Y. and Shin, S.J.
학회지명
Journal of Aerospace Engineering, Accepted 2026.
SCI 순위
[Clarivate JCR] ENGINEERING, AEROSPACE - SCIE: 상위 42.7%
123
Design and Comparison of a Tiltwing eVTOL for a Different Rotor Sizing
연구자
Choi, H.R., Chang, B.Y., Jo, Y. and Shin, S.J.
학회지명
Journal of Aircraft, Accepted 2026.
SCI 순위
[Clarivate JCR] ENGINEERING, AEROSPACE - SCIE: 상위 29.63%
122
Design of Lift Plus Cruise eVTOL Aircraft with Initial Fuselage Frame Design
연구자
Kim, A.R., Cha, W.S., Park, S.H., Ahn, C., Chang, B.Y., Choi, K. and Shin, S.J.
학회지명
International Journal of Aeronautical and Space Sciences, Accepted 2026.
SCI 순위
[Clarivate JCR] ENGINEERING, AEROSPACE - SCIE: 상위 50%
121
Comprehensive Maneuver Load Analysis of a Hingeless Coaxial Rotorcraft for Blade Structural Design
연구자
Kong, K., Im, B., Kim, S., Lee, H., Ko, G., Ryi, J., and Shin, S.J.
학회지명
International Journal of Aeronautical and Space Sciences, Published Online, 2026.
SCI 순위
[Clarivate JCR] ENGINEERING, AEROSPACE - SCIE: 상위 50%
120
A localized version of the dual-primal finite element tearing and interconnecting method for the partitioned analysis of heterogeneous structural systems
연구자
González, J.A., Kang, S.-H., Kim, H.H., Shin, S.J., and Park, K.C.
학회지명
International Journal for Numerical Methods in Engineering, Vol. 127, No. 2, 2026.
SCI 순위
[Clarivate JCR] ENGINEERING, MULTIDISCIPLINARY - SCIE: 상위 24.3%
DOI
https://doi.org/10.1002/nme.70265
119
Solving FEM Models without assembly: its Promise and Challenge
연구자
Park, K. C., González, J. A., Shin, S. J., Kang, S. H., Hwang, M. H., Kim, J. G., Baqir, F., Han, J. H., Hagos, R. W., Lee, S. C., Park, Y. H., Kim, H
학회지명
Computer Methods in Applied Mechanics and Engineering, Vol. 450, 118588, 2026.
SCI 순위
[Clarivate JCR] MATHEMATICS, INTERDISCIPLINARY APPLICATIONS - SCIE: 상위 3.3%
DOI
https://doi.org/10.1016/j.cma.2024.117155
118
Improved method for measuring the impact response of a composite rotor blade