Evaluation of geometric conservation law using pressure‐based fluid solver and moving grid technique

DOI10.1108/09615530410546254zbMath1075.76043OpenAlexW2030858057MaRDI QIDQ5699613

Wei Shyy, R. Kamakoti

Publication date: 26 October 2005

Published in: International Journal of Numerical Methods for Heat & Fluid Flow (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1108/09615530410546254

zbMATH Keywords

Jacobianfinite volume methods2D channel3D elastic wing

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Gas dynamics (general theory) (76N15)

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Cites Work

• Unnamed Item
• Geometric conservation laws for flow problems with moving boundaries and deformable meshes, and their impact on aeroelastic computations
• Second-order time-accurate and geometrically conservative implicit schemes for flow computations on unstructured dynamic meshes
• On the significance of the geometric conservation law for flow computations on moving meshes
• Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
• Low Reynolds number turbulent flows around a dynamically shaped airfoil
• Geometric Conservation Law and Its Application to Flow Computations on Moving Grids
• The discrete geometric conservation law and the nonlinear stability of ALE schemes for the solution of flow problems on moving grids.