Titlebook: Separated Flows and Jets; IUTAM-Symposium, Nov V. V. Kozlov,A. V. Dovgal Conference proceedings 1991 Springer-Verlag, Berlin Heidelberg 199

ASSET

Effects of 3-D Surface Mounted Obstacles on Marginal Separations is placed on the discussion of the resulting wall streamline pattern. Numerical solutions of the solvability condition which describes the local interaction between the boundary layer and the external inviscid flow are presented for a one parameter family of hills/dents whose height varies slowly

Hla461

inveigh

Computation of Trailing-Edge Separation Using an Accelerated, Updated Bluff-Body, Interacting Boundafully asymmetric, although only symmetric profiles are addressed in this study (primarily the NACA00xx series). The interacting boundary layer algorithm is based on a bluff-body formulation that linearizes the thin airfoil integrals about some known exact inviscid baseline solution. The present form

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Self-Similar Separationws of viscous fluid are considered including effects of buoyancy and electric conductivity. Regions of near-wall separation or recirculation zones inside of a motion region appear which are bounded by conical surfaces. Particularly, problems on a vortex-source flow in free space and near a wall, mul

门窗的侧柱

消毒

chondromalacia

发起

On Goldstein’s Singularity airfoils at incidence. But full clarity in the issue at hand was not achieved, that is why it seems expedient to treat the Goldstein’s solution as a limiting one in a more general class of functions depending on a similar veritable and including singular pressure distribution.

ANT

Marginal Separation Theoryupersonic boundary layer separation on cold surface. It is shown that depending on mean Mach number taken across the boundary layer two versions of the theory may be constructed. In the first case boundary layer separates through the removal of Goldstein’s singularity. In the second one the marginal separation theory rules over the process.

AMPLE