A numerical solution is presented for the two-dimensional inviscid incompressible separated flow over a heated flat semi-infinite plate with a square leading edge aligned normal to the flow. The instantaneous flow velocity field is computed using a discrete-vortex model. The instantaneous thermal field is calculated via a third-order upwind differencing technique. Augmentation of the time-average Nusselt number is found to occur as the mean reattachment length is shortened through application of a transverse sound field.
|Title of host publication
|Computational Techniques and Applications: CTAC-85
|John Noye, Robert May
|Number of pages
|Published - 1 Dec 1986