Publication Date:
2019-07-13
Description:
The unsteady, compressible, thin-layer Navier-Stokes equations are used to obtain three-dimensional, asymmetric, vortex-flow solutions around cones and cone-cylinder configurations. The equations are solved using an implicit, upwind, flux-difference splitting, finite-volume scheme. The computational applications cover asymmetric flows around a 5 semi-apex angle cone of unit length at various Reynolds number. Next, a cylindrical afterbody of various length is added to the conical forebody to study the effect of the length of cylindrical afterbody on the flow asymmetry. All the asymmetric flow solutions are obtained by using a short-duration side-slip disturbance.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
Asian Pacific Conference on Computational Mechanics; Dec 11, 1991 - Dec 13, 1991; Hong Kong|Old Dominion Univ., Analysis and Control of Asymmetric Vortex Flows and Supersonic Vortex Breakdown; 8 p
Format:
application/pdf
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