Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies

DOI10.1016/0045-7930(94)00040-6zbMath0838.76051OpenAlexW2101806978WikidataQ127212549 ScholiaQ127212549MaRDI QIDQ1905642

Yanyan Li

Publication date: 3 June 1996

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://digitalcommons.calpoly.edu/aero_fac/1

zbMATH Keywords

\(k\)-epsilon turbulence modelbody boattail anglegolden section optimization methodMacCormack unsplit explicit algorithmmass-average Navier-Stokes equations

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Shear flows and turbulence (76F10) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20)

Related Items (4)

Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies ⋮ Finite element/volume solution to axisymmetric conservation laws ⋮ Node-pair finite volume/finite element schemes for the Euler equation in cylindrical and spherical coordinates ⋮ A multislope MUSCL method on unstructured meshes applied to compressible Euler equations for axisymmetric swirling flows

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• Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies
• Numerical study of the turbulent flow past an airfoil with trailing edge separation
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• Computation of high speed turbulent boundary-layer flows using thek-ε turbulence model
• Computation of a Supersonic Flow Past an Axisymmetric Nozzle Boattail with Jet Exhaust

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