A numerical study of tuned liquid damper based on incompressible SPH method combined with TMD analogy

2018 ◽  
Vol 82 ◽  
pp. 394-411 ◽  
Author(s):  
Armin Hajighasem Kashani ◽  
Amir Mahdi Halabian ◽  
Keyvan Asghari
2021 ◽  
Vol 242 ◽  
pp. 110129
Author(s):  
Meng-Chang Hsieh ◽  
Guan-Lee Huang ◽  
Haijun Liu ◽  
Shih-Jiun Chen ◽  
Bang-Fuh Chen

2021 ◽  
pp. 1-31
Author(s):  
Kevin P. McNamara ◽  
Michael J. Tait

Abstract The tuned liquid damper (TLD) is a system used to reduce the response of tall structures. Numerical modelling is a very important tool when designing TLDs. Many existing numerical models are capable of accurately capturing the structure-TLD system response at serviceability levels, covering the range where TLDs are primarily intended to perform. However, these models often have convergence issues when considering more extreme structural excitations. The goal of this study is to develop a structure-TLD model without convergence limitations at large amplitude excitations. A structure-TLD numerical model where the TLD is represented by a 2D incompressible SPH scheme is presented. The TLD contains damping screens which are represented by a force term based on the Morison equation. The performance of the model is assessed by comparing to experimental data for a structure-TLD system undergoing large amplitude excitations consisting of four-hour random signals and shorter transient signals. The model shows very good agreement with the experimental data for the structural response. The free surface response of the TLD is captured accurately by the model for the lower excitation forces considered, however as the excitation force is increased there are some discrepancies. The large amplitude excitations also result in SPH fluid particles penetrating the boundaries, resulting in degradation of the model performance over the four-hour simulations. Overall, the model is shown to capture the response of a structure-TLD system undergoing large amplitude excitations well.


2015 ◽  
Vol 126 ◽  
pp. 660-664 ◽  
Author(s):  
Xi-Peng Lv ◽  
Xing Zheng ◽  
Ni-Bo Zhang ◽  
Kang-Ning Niu

2008 ◽  
Vol 40 (9) ◽  
pp. 637-661 ◽  
Author(s):  
B Ataie-Ashtiani ◽  
G Shobeyri ◽  
L Farhadi

Author(s):  
Amirsaman Farrokhpanah ◽  
Javad Mostaghimi

Multiphase Smoothed Particle Hydrodynamics (SPH) method has been used to study the jet breakup phenomena. It has been shown that this method is well capable of capturing different jet breakup characteristics. The value obtained for critical Weber number here in transition from dripping to jetting is a very good match to available values in literature. Jet breakup lengths are also agreeing well with several empirical correlations. Successful usage of SPH, as a comparably fast CFD solver, in jet breakup analysis helps in speeding up the numerical study of this phenomenon.


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