One-Dimensional Test Setup
First investigations were carried out with one-dimensional test configurations loosely following an approach laid out by Jaiman et al. [17]: The one-dimensional fluid mesh and the structural mesh are colinear, but feature non-matching discretisations. An analytical pressure distribution is applied to the fluid mesh. The equivalent consistent nodal loads are then projected on the structural nodes. Furthermore, a reference load distribution can be obtained by calculating the nodal loads consistent with the pressure distribution directly at the structural nodes. The reference loads can then be used to calculate a relative error eF of the projected loads. In the first three diagrams of Fig. 6, the analytical pressure distribution is plotted over the length of the one-dimensional domain together with the forces acting on the fluid nodes and on the structural nodes. The fluid mesh is discretised with an increasing number of elements nCFD, whereas the number of elements on the structural side is kept constant at nCSD = 20. In this example, linear shape functions are used for both the calculation of the consistent nodal forces and for their projection with the FIE method. With the coarser CFD meshes the distribution of the projected forces on the structural nodes is highly irregular. Parameter studies indicate that the mesh spacings on
Fig. 6 Influence of the mesh ratio on the load distribution on a one-dimensional test configuration. top left, top right and bottom left: Consistent nodal forces on the fluid nodes and projected forces on the structural nodes for fluid meshes with 9, 13 and 17 elements. The number of structural elements is kept at nCSD = 20. bottom right: Relative error £F plotted over the mesh ratio y. |
both sides have to be fairly similar in order to achieve a sufficiently regular load distribution. The graph on the bottom right of Fig. 6 underscores this result. It shows the relative error plotted over the mesh ratio у = i+^csD/wcro’ Values from -1 to 0 imply a fluid mesh coarser than the structural mesh, and values between 0 and 1 a finer one. For negative values of у the error is high, and only approaching у = 0 it decreases to an acceptable level. In this example, for у = 0 the structural nodes and the fluid nodes are placed at the same coordinates and the relative error becomes zero (not shown in the logarithmic diagram).