Efficient nonlinear static aeroelastic wing analysis
DOI10.1016/S0045-7930(98)00047-4zbMath0970.76062MaRDI QIDQ1973762
Perry A. Newman, J. C. III Newman, Arthur C. III. Taylor, Gene J.-W. Hou
Publication date: 20 September 2000
Published in: Computers and Fluids (Search for Journal in Brave)
finite elementsstressstructural analysisnonlinear Euler equationsflexible wingunstructured tetrahedral meshesstructural deflectionsupwind cell-centered finite-volume scheme
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05) Finite volume methods applied to problems in fluid mechanics (76M12) Gas dynamics (general theory) (76N15)
Cites Work
- Development of a multigrid code for 3-D Navier-Stokes equations and its application to a grid-refinement study
- Aeroelastic time response analysis of thin airfoils by transonic code LTRAN 2
- An implicit upwing algorithm for computing turbulent flows on unstructured grids
- Dynamic unstructured method for flows past multiple objects in relative motion
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