An adaptive grid method for analysis of 3D aircraft configurations

DOI10.1016/0045-7825(92)90024-EzbMath0778.76050OpenAlexW2050918440MaRDI QIDQ686948

Craig L. Hilmes, Michael B. Bieterman, Robin G. Melvin, David P. Young, Forrester T. Johnson, John E. Bussoletti

Publication date: 17 October 1993

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(92)90024-e

zbMATH Keywords

error indicatorsdesign problemscode TRANAIRlocal rectangular finite elements

Mathematics Subject Classification ID

Finite element methods applied to problems in fluid mechanics (76M10) Mesh generation, refinement, and adaptive methods for boundary value problems involving PDEs (65N50) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (2)

A local grid refinement technique based upon Richardson extrapolation ⋮ Error estimates and adaptive finite element methods

Cites Work

• A locally refined rectangular grid finite element method: Application to computational fluid dynamics and computational physics
• Entropy Condition Satisfying Approximations for the Full Potential Equation of Transonic Flow
• Conservative calculations of non-isentropic transonic flows
• Global convergence of inexact Newton methods for transonic flow

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