scholarly journals Experimental study of cactus-like body shape on flow-induced vibration mitigation of clustered cylinders

Author(s):  
Chen Shi ◽  
Yang Liu ◽  
Jialu Wang ◽  
Fabo Chen ◽  
Zhihui Liu ◽  
...  
Author(s):  
Lixia Gao ◽  
Jie Yang ◽  
Zilong Jiang ◽  
Jianzhong Ma ◽  
Song Li

In this paper, the Flow Induced Vibration (FIV) tests of heat transfer helical tube bundle have been carried out. The results show that the more large flow velocity in tube becomes, the more high pressure drop of bundle is. The dynamic buckling of bundle does not occur during steady-state operation. The fatigue evaluation has been done according to ASME code and the structure is founded to satisfy the ASME code requirements.


2001 ◽  
Vol 67 (654) ◽  
pp. 349-356
Author(s):  
Takuzo IWATSUBO ◽  
Shozo KAWAMURA ◽  
Mureithi W.Njuki ◽  
Takahiro SHIBUYA

1999 ◽  
Vol 125 (9) ◽  
pp. 977-986 ◽  
Author(s):  
Y. L. Xu ◽  
S. Zhan ◽  
J. M. Ko ◽  
Z. Yu

2022 ◽  
Vol 23 (1) ◽  
pp. 358-369
Author(s):  
Nur Ain Shafiza Ramzi ◽  
Kee Quen Lee ◽  
NUR AMIRA BALQIS MOHD ZAINURI ◽  
HOOI SIANG KANG ◽  
NOR’AZIZI OTHMAN ◽  
...  

An experimental study was carried out to identify the effect of angle of attack on flow-induced vibration (FIV) of square cylinders. The experiment was conducted at the Aeronautical and Wind Engineering Laboratory (AEROLAB), UTM Kuala Lumpur using a wind tunnel that was free from external wind conditions. A supporting structure was designed and fabricated to conduct this experiment. The importance of this support structure was to enable the rigid cylinder to suspend and vibrate freely upon excitation of wind speed. The results were analysed through the response of amplitude and frequency of the rigid cylinder over a velocity range of 0.5m/s to 4.0m/s. The results showed that for a square cylinder of ?=0°, vortex-induced vibration (VIV) occurred at low reduced velocity (UR) in range of 5 ? UR ? 10 and galloping occurred at higher reduced velocity which started at UR=15. A tranquil zone was found between VIV and galloping in the reduced velocity range of 10 ? UR ? 15. As for ?=22.5° and 45°, only VIV response was found at low reduced velocity in range of 4? UR ? 9. ABSTRAK: Satu kajian eksperimentasi telah dilakukan bagi mengenal pasti pengaruh sudut serangan oleh getaran cetusan-aliran (FIV) dalam silinder persegi. Eksperimen ini dijalankan di Makmal Kejuruteraan Aeronautika dan Angin (AEROLAB), UTM Kuala Lumpur dengan menggunakan terowong angin yang bebas dari pengaruh angin luar. Struktur sokongan telah direka dan difabrikasi bagi tujuan eksperimen ini. Ini penting bagi membolehkan silinder pegun tergantung dan bergetar dengan bebas semasa ujian kelajuan angin. Dapatan kajian dianalisis melalui tindak balas amplitud dan frekuensi silinder pegun pada kadar halaju 0.5m/s sehingga 4.0m/s. Hasil kajian menunjukkan bahawa bagi silinder persegi ? = 0 °, getaran pengaruh-vorteks (VIV) berlaku pada halaju rendah (UR) dalam julat 5 ? UR ? 10 dan getaran lebih teruk telah ketara berlaku pada kadar halaju berkurang iaitu bermula pada UR = 15. Zon tenang dijumpai antara VIV dan getaran teruk pada kadar halaju berkurang 10 ? UR ? 15. Adapun pada ? = 22.5° dan 45°, hanya tindak balas VIV dijumpai pada halaju rendah dalam kadar 4? UR ? 9.


2018 ◽  
Vol 169 ◽  
pp. 492-510 ◽  
Author(s):  
Wanhai Xu ◽  
Shuhai Zhang ◽  
Bin Liu ◽  
Enhao Wang ◽  
Yin Bai

2001 ◽  
Vol 67 (660) ◽  
pp. 2484-2490
Author(s):  
Masahiro WATANABE ◽  
Kenichi NAKANISHI ◽  
Nobuyuki KOBAYASHI ◽  
Fumio HARA

2007 ◽  
Vol 21 (9) ◽  
pp. 1359-1366 ◽  
Author(s):  
Y. S. Choya ◽  
J. Huang ◽  
L. Huang ◽  
Y. Zhou

2019 ◽  
Vol 349 ◽  
pp. 8-19 ◽  
Author(s):  
Zhengting Quan ◽  
Kefeng Zhang ◽  
Zhenqin Xiong ◽  
Hongbiao Zu ◽  
Hanyang Gu ◽  
...  

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