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Results of computations of aerodynamic flows with attached and separated boundary layers with adverse pressure gradients are presented. The objective is to compare the predictive accuracy of 11… (More)
Les methodes numeriques discretes pour la resolution des equations de Navier Stokes ne necessitent pas seulement des conditions aux limites de paroi solide classique mais egalement une valeur de la… (More)
Abstract A new finite difference solution for Prandtl's boundary-layer equations is described in detail for steady, incompressible luminar and turbulent flows. Only boundary sheets will be considered… (More)
It is well-known that boundary-layer theory cannot be applied to the prediction of the complete flow field past an aircraft configuration, because the boundary-layer approach is not valid, for… (More)
In Sub-Section 4.3.1 we have seen that if the Reynolds number characterizing a flow field is large enough, we can separate the flow field into inviscid and viscous portions. From Fig. 2.3, Section… (More)
The 12 papers in this conference have been previously abstracted in NSA. Abstract numbers for these papers can be found under CONF-700557 in the NSA Report Number Index. (TFD)