viv of a rigid cylinder near a plane subjected to steady subcritical flow
Table
Table of Contents
1 table
viv of a cylinder near a plane boundary
governing and influencing parameters:
- Re(flow regimes)
- G/D
- m*ξ (Govardhan & Williamson 2006)
- BL(laminar, turbulent, thickness/G)
8.3.2 sumer, 1997
Authors, year | DOF | m*ξ | ξ | Re | flow regime | G/D | BL | Current | waves kc | methods | New | Methods | Ur | independent variables | dependent variables | ref | |
Chern, 2018 | 200 | laminor | effect of viv on plane boudnary(skin friction) | Num. 2D, 2DOF | 412 | G/D, Ur | X, Y,Cf, fv/fn, trajectory | 1 | |||||||||
A.Munir, 2018, | 5000 | subcritical(TrSL) | 2DOF, near plane, osciallatory flow | num. 2D, 2DOF | kc,5,10 ; G/D,0.01, .4, 1. \infity | ||||||||||||
Barbosa, 2017 | 7250, 10,000, 12,500, 15,500 | subcritical | |||||||||||||||
Hsieh, 2016 | 3036~3924 | subcritical | |||||||||||||||
Chung, 2016 | 100 | laminor | |||||||||||||||
khalak and Williamson,1997 | 2 | 0.0108,0.00858,0.0135 | steady | - | exp. |
- flow regime, refer to 1-1, zdravkovich,1997
- DOF : degree of freedom
ref:
- table 10.1 sumer,1997{B}
- where, B means book
1.1 validation
stationary cylinder no plane boundary
The velocity field of the turbulent very near wake of a circular cylinder
By:Ong, L (Ong, L); Wallace, J (Wallace, J)
1.2 khalak and Williamson,1997, JFS
NEW input variables: Very low m*ξ Q?
- what is the dominant response frequency during excitation
- lock-in region
- A* vs. Ur
exp. U* = U/fn D, where fn is the natural frequency of the structure in water
2 setups
- all setups are the same as Khalak and Williamson 1997 except add a plane boundary
- Re(1e3, 1e4)
vibration-system
- low M* (<6)
3 new contribution from guo fei
- flow field properties
- higher Re, others work mostly on laminar (# not great new, lots of work on subcritical flow regime)
- 3D rather than 2D
- non-linearity
- wider G/D
4 english
intermittent {adj}
occurring at irregular intervals; not continuous or steady. "intermittent rain"
Footnotes:
1
DEFINITION NOT FOUND.