Publication Date:
2019-07-13
Description:
The unsteady boundary layer due to a single rectilinear vortex filament approaching a 2-D stagnation point is investigated. Assuming the vortex remains far from the surface, incompressible potential flow theory is used to determine the time dependent inviscid flow field. The unsteady boundary layer equations are solved by an alternating-direction-implicit finite-difference method. Two mechanisms which cause fluctuations in heat transfer are the unsteady velocity field in the boundary layer and secondly, the unsteady total temperature at the edge of the boundary layer. The relative importance of these mechanisms is dependent upon the total temperature fluctuations relative to the imposed temperature difference. As a vortex approaches a stagnation point it may be forced to one side of the stagnation line or the other, depending on its initial position. Results are presented for both of these cases.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
NASA-CR-182297
,
E-4834
,
NAS 1.26:182297
,
AIAA PAPER 89-1690
,
Thermophysics Conference; Jun 12, 1989 - Jun 14, 1989; Buffalo, NY; United States
Format:
application/pdf
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