Computational model of flexible membrane wings in steady laminar flow

DOI10.2514/3.12811zbMath0858.73064OpenAlexW2091912777MaRDI QIDQ4878238

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Publication date: 23 March 1997

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

Full work available at URL: https://doi.org/10.2514/3.12811

zbMATH Keywords

convergenceiterative procedureperfect fluidequilibrium configurationsaerodynamic characteristicsaerodynamic pressurecircular arc airfoilgrid approximation methodnormal tensioniterative recalculation of nodesshearing tensiontangent loading

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20)

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Finite element computations for unsteady fluid and elastic membrane interaction problems ⋮ Aeroelastic analysis of membrane airfoils and flexible-chord airfoils with trailing-edge flaps ⋮ Thrust, drag and wake structure in flapping compliant membrane wings ⋮ Flow-excited membrane instability at moderate Reynolds numbers ⋮ Computation of unsteady laminar flow over a flexible two-dimensional membrane wing ⋮ Computation of aerodynamic coefficients for a flexible membrane airfoil in turbulent flow: A comparison with classical theory ⋮ A biologically inspired micro-vehicle capable of aerial and terrestrial locomotion

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