Yi-Ren Wang

Prof. Yi-Ren Wang

Aerospace Engineering, Tamkang University, Taipei, Taiwan
+1
orcid

Research Focus & Metrics

Academic Career Length

31Years (1996-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 March 2015 in Journal of Applied Mechanics and Technical Physics
Verified
Journal Article
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Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
ZFZhi-Wei Fang
Zhi-Wei Fang
Vibrations in an elastic beam supported by nonlinear supports at both ends under the influence of harmonic forces are analyzed in this study. It is hypothesized that the elastic Bernoulli-Euler beam is supported by cubic springs to simulate nonlinear boundary conditions. The dynamic behavior of the beam is described by using the Fourier expansion and the Bessel functions. The Hankel transform is then applied to obtain particular (nonhomogeneous) solutions. This study succeeds in describing the “jump” phenomenon (instantaneous transition of the system from one position to another) of the vibrating system at certain frequencies. Models based on linear boundary conditions are unable to capture this phenomenon. A larger modulus of elasticity in nonlinear supports increases the frequency of unstable vibrations in the first mode and also widens the frequency region of system instability. This influence is less prominent in the second mode, in which the largest amplitude is smaller than those observed in the first mode.

1 September 2018 in Journal of Sound and Vibration
Verified
Journal Article
Closed access
Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
CFC.K. Feng
C.K. Feng
SCS.Y. Chen
S.Y. Chen

1 August 2015 in Journal of Sound and Vibration
Verified
Journal Article
Closed access
Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
TLTzu-Wen Liang
Tzu-Wen Liang

3 February 2015 in International Journal of Structural Stability and Dynamics
Verified
Journal Article
Closed access
Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
KHKo-En Hung
Ko-En Hung

5 November 2021 in Sensors
Verified
Journal Article
Open access
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Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
MCMing-Ching Chu
Ming-Ching Chu
This research proposes an energy harvesting system that collects the downward airflow from a helicopter or a multi-axis unmanned rotary-wing aircraft and uses this wind force to drive the magnet to rotate, generating repulsive force, which causes the double elastic steel system to slap each other and vibrate periodically in order to generate more electricity than the traditional energy harvesting system. The design concept of the vibration mechanism in this study is to allow the elastic steel carrying the magnet to slap another elastic steel carrying the piezoelectric patch to form a set of double elastic steel vibration energy harvesting (DES VEH) systems. The theoretical DES VEH mechanism of this research is composed of a pair of cantilever beams, with magnets attached to the free end of one beam, and PZT attached to the other beam. This study analyzes the single beam system first. The MOMS method is applied to analyze the frequency response of this nonlinear system theoretically, then combines the piezoelectric patch and the magneto-electric coupling device with this nonlinear elastic beam to analyze the benefits of the system’s converted electrical energy. In the theoretical study of the DES VEH system, the slapping force between the two elastic beams was considered as a concentrated load on each of the beams. Furthermore, both SES and DES VEH systems are studied and correlated. Finally, the experimental data and theoretical results are compared to verify the feasibility and correctness of the theory. It is proven that this DES VEH system can not only obtain the electric energy from the traditional SES VEH system but also obtain the extra electric energy of the steel vibration subjected to the slapping force, which generates optimal power to the greatest extent.

1 April 2016 in Journal of Engineering Mechanics
Verified
Journal Article
Closed access
Yi-Ren WangYi-Ren Wang
Yi-Ren Wang
TKTing-Hung Kuo
Ting-Hung Kuo
This study examined the vibrations of a hinged-free nonlinear beam placed on a nonlinear elastic foundation. The authors found that specific combinations of an elastic modulus in the elastic foundation resulted in 1:3 internal resonances in the first and second modes of the beam. This prompted adding a dynamic vibration absorber (DVA) on the elastic beam in order to prevent internal resonance and suppress vibrations. When the DVA was placed at the free end of the beam, the boundaries were time dependent. Thus, a shifting polynomial function was used to convert the nonhomogeneous boundary conditions into homogeneous boundary conditions. The authors analyzed this nonlinear system using the method of multiple scales (MOMS). Fixed-point plots were also used to facilitate the observation of internal resonance. This made it possible to study the influence of nonlinear geometry and nonlinear inertia associated with the vibration of the elastic beam. The authors also examined the combination of optimal ma...