Computation of the asymmetric vortex pattern for bodies of revolution

DOI10.2514/3.8280zbMath0524.76042OpenAlexW2059173442MaRDI QIDQ3036959

No author found.

Publication date: 1983

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.8280

zbMATH Keywords

angle of attackthree-dimensionalsymmetric vorticesslender body of revolutionangle of attack of 30 degCRAY-1 computerlaminar flow assumptionleeside vortex patternMacCormack's algorithmMach number 1.6three-caliber ogive cylinder at Mach number 1.98 angle of attack of 20 degvectorized

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Basic methods in fluid mechanics (76M99)

Related Items (3)

Flow field saddles and their relation to vortex asymmetry ⋮ Numerical investigation of the mechanism of asymmetric vortex flows ⋮ Numerical issues affecting vortex asymmetries computed with the conical Navier-Stokes equations

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