Space marching calculations about hypersonic configurations using a solution-adaptive mesh algorithm

DOI10.2514/3.11853zbMath0782.76073OpenAlexW2092145515MaRDI QIDQ4274162

S. L. Lawrence, Albert D. Harvey III, Sumanta Acharya

Publication date: 24 February 1994

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

Full work available at URL: https://doi.org/10.2514/3.11853

zbMATH Keywords

angles of attackall-body-type geometryblended-wing-body designelliptical cross sectionsthree-dimensional parabolized Navier-Stokes equation

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Mesh generation, refinement, and adaptive methods for boundary value problems involving PDEs (65N50) Mesh generation, refinement, and adaptive methods for the numerical solution of initial value and initial-boundary value problems involving PDEs (65M50) Hypersonic flows (76K05)

Related Items (2)

Solution-adaptive techniques in computational heat transfer and fluid flow ⋮ Space-marching method for calculating steady supersonic flows on a grid adapted to the solution

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