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Numerical Solution of Viscous Flows about Submerged and Partly Submerged Bodies
Pages 607-616

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From page 607...
... Experimental investigation can provide global information at reasonable cost, while velocity and pressure measurement are difficult or even impossible and very expensive, instead numerical simulation gives the complete flow field quantities provided particular care is devoted to implement the numerical scheme. The validation of the numerical solution by a comparison with the experimental findings is necessary to verify the accuracy of scheme.
From page 608...
... The choice of Cartesian velocity components as dependent variables allows a simple form of the equations in the (I coordinate system. The adoption of other velocity components as unknowns require the introduction of higher order metric coefficients, as shown in Ref.
From page 609...
... 5 Results To test the complexities associated with the described numerical scheme, several cases have been chosen, each one enlighting a particular complexity. The flow in a steady domain and the flow in a domain where a boundary moves with a prescribed law have been considered as test cases before solving the free surface flow past a semicylinder.
From page 610...
... These preliminary numerical results assess that the numerical model provides good flow simulation in presence of steady and unsteady irregular domains. 5.3 Free surface flows free surface flows involve the difficulty of irregular and time dependent domain, where boundary moves according to the velocity field.
From page 611...
... Numerical Solution of 3-D Flows Periodic in One Direction and with Complex Geometries in 2-D" unpublished t9; Beam R.M., Warming R.F., "An Implicit FiniteDifference Algorithm for Hyperbolic Systems in Conservation-Law Form" J
From page 612...
... "Finite Difference Computations Using Boundary-fitted Coordinates for Free-surface Potential Flows Generated by Submerged Bodies" in Proceedings of the 2r~d Ir~tern.
From page 613...
... t =0.3 t = 0.4 t=O.S t=0.6 A t =0.7 E t =0.8 t =0.9 t = 1.0 Fig. 3 Instantaneous streamline plots within one period for the Dow in channel with a moving indentation 613
From page 614...
... C and D for the flow in a channel with a moving indentation 614 ~7 l 1 i 1 1 2 3 4 5 6 · Exper. ~ Numer.
From page 615...
... 6 Pressure contour map at t=0.8, Re = 400, Fr = 0.5 for the flow over a semicylindrical bump. The increment between two isolines is O.OS 615


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