Blind predictions of laboratory measurements of vortex-induced vibrations of a tension riser

被引:249
作者
Chaplin, JR [1 ]
Bearman, PW
Cheng, Y
Fontaine, E
Graham, JMR
Herfjord, K
Huera-Huarte, FJ
Isherwood, M
Lambrakos, K
Larsen, CM
Meneghini, JR
Moe, G
Pattenden, R
Triantafyllo, MS
Willden, RHJ
机构
[1] Univ Southampton, Sch Civil & Environm Engn, Southampton, Hants, England
[2] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London, England
[3] Technip, Houston, TX USA
[4] Inst Francais Petr, F-92506 Rueil Malmaison, France
[5] Norsk Hydro Oil & Energy, Bergen, Norway
[6] Orcina Ltd, Ulverston, England
[7] Norwegian Univ Sci & Technol, Dept Marine Technol, N-7034 Trondheim, Norway
[8] Univ Sao Paulo, Escola Politecn, Dept Mech Engn, Sao Paulo, Brazil
[9] Norwegian Univ Sci & Technol, Dept Civil & Transport Engn, N-7034 Trondheim, Norway
[10] MIT, Dept Ocean Engn, Cambridge, MA 02139 USA
基金
英国工程与自然科学研究理事会;
关键词
vortex-induced vibrations; riser; CFD; numerical modelling; blind predictions; multi-mode response;
D O I
10.1016/j.jfluidstructs.2005.05.016
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper compares laboratory measurements of the vortex-induced vibrations of a riser in a stepped current with blind predictions obtained with I I different numerical models. Results are included oil in-line and transverse displacements and curvatures, and dominant frequencies. In general, empirical models were more successful at predicting cross-flow displacements and Curvatures than Current codes based oil CFD. Overall ratios between predictions and measurements of cross-now displacements were around 95% and 75%, respectively. Predictions of cross-flow curvatures were more scattered, and almost all were unconservative. In-line vortex-induced curvatures, which may cause as much damage as cross-flow curvatures, could not be computed by any of the empirically based codes, and in general those based oil CFD were in very poor agreement with the measurements. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:25 / 40
页数:16
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