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Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies
2005
43rd AIAA Aerospace Sciences Meeting and Exhibit
unpublished
A three-dimensional Euler solver is used to study the vortex core over slender conical bodies at high angles of attack and low speeds. A three-dimensional conical overset-grid is established to reduce the computational efforts while accurately resolve the vortex flow. The numerical results on the vortex core are verified by available experimental data and theoretical solutions. The line vortex model used in the theoretical stability analyses made by the present authors for the vortex flow is
doi:10.2514/6.2005-62
fatcat:3uhstjh6u5f7tbag7jiuxntwru