Abstract
Motivated by devices such as the atomic force microscope, we compute the drag experienced by a cylindrical body of circular or rectangular cross-section oscillating at small amplitude near a plane wall. The body lies parallel to the wall and oscillates normally to it; the body is assumed to be long enough for the dominant flow to be two-dimensional. The flow is parameterized by a frequency parameter γ2 and the wall-body separation δ (scaled on body radius). Numerical solutions of the unsteady Stokes equations obtained using finite-difference computations in bipolar coordinates (for circular cross-sections) and boundary-element computations (for rectangular cross-sections) are used to determine the drag on the body. Numerical results are validated and extended using asymptotic predictions (for circular cylinders) obtained at all extremes of (γ, δ)-parameter space. Regions in parameter space for which the wall has a significant effect on drag are identified. © 2005 Cambridge University Press.
Original language | English |
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Pages (from-to) | 397-426 |
Number of pages | 29 |
Journal | Journal of Fluid Mechanics |
Volume | 545 |
DOIs | |
Publication status | Published - 25 Dec 2005 |