Jinbin Wen
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Research Interests
Jinbin Wen has a total of 4 co-authors. Here are the top co-authors by number of shared publications:
- Dan Zhao
Potsdam Institute for Climate Impact Research 3 , Potsdam 14412
1 shared publication - Qi Liu
Institute of Science Tokyo
1 shared publication - Weili Guo
School of Mathematics and Statistics, Northwestern Polytechnical University, Xi’an 710072, P. R. China
1 shared publication - Yong Xu
School of Mathematics and Statistics, Northwestern Polytechnical University, Xi’an, China
1 shared publication
Latest Publications
- 3 March 2026
- Published by World Scientific Pub Co Pte Ltd in International Journal of Bifurcation and Chaos
- Vol. 36 (08)
Noise-Enhanced Stabilization and Reliability for a Z-Shaped Folding Wing
A stochastic dynamic model is proposed for a Z-shaped folding wing with random excitations. The method of multiple scales is employed to derive amplitude equations. Bistable phenomenon on the deterministic system is revealed through analyses on bifurcation and basin of attraction. Under the effect of random loads, the noise-induced transition behavior is observed, and the noise-enhanced stabilization phenomenon is examined in detail. Reliability analysis is conducted using a proposed reliability index. Reliability region is presented versus different parameters including noise intensity. The results of this study can provide guidance for the design and reliability analysis of folding wings.
- 3 March 2026
- Published by World Scientific Pub Co Pte Ltd in International Journal of Bifurcation and Chaos
- Vol. 36 (08)
Noise-Enhanced Stabilization and Reliability for a Z-Shaped Folding Wing
A stochastic dynamic model is proposed for a Z-shaped folding wing with random excitations. The method of multiple scales is employed to derive amplitude equations. Bistable phenomenon on the deterministic system is revealed through analyses on bifurcation and basin of attraction. Under the effect of random loads, the noise-induced transition behavior is observed, and the noise-enhanced stabilization phenomenon is examined in detail. Reliability analysis is conducted using a proposed reliability index. Reliability region is presented versus different parameters including noise intensity. The results of this study can provide guidance for the design and reliability analysis of folding wings.