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Fig.A-1
An example of flow which cannot be computed andevaluated by the present approach because its computation re- presents a two-dimensional problem: vortices visualised in slow (velocity only 14 mm/s) flow past a cylinder. |
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Fig.A-2 Decomposition
of an aeroplane surface into elements used innumerical three-dimensional flowfield computations (Avions Marcel Dassault, France). |
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Vaclav TESAR : "BASIC FLUID MECHANICS"