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- W2321442237 abstract "In our previous work, a strong-coupling approach was successfully used to simulate highly flexible wings interacting with surrounding fluid flows in a globally Eulerian framework for both fluid and solid. However there was a strong assumption to simplify the formulation: the wing structure has the same density as the surrounding fluid. Here, using a fast-tracking method to efficiently identify the solid and fluid areas and solving modified momentum equations and pressure Poisson equation with variable (but still incompressible) density, we were able to apply the same idea to solve flapping-wing system with arbitrary density ratio. In the investigation of effects by different density ratio, for the same shear modulus, higher structural density actually leads to a “softer” appearance with larger deformation of the wing, as a result of relatively stronger inertial effect. Meanwhile, the wake" @default.
- W2321442237 created "2016-06-24" @default.
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- W2321442237 date "2011-01-04" @default.
- W2321442237 modified "2023-10-02" @default.
- W2321442237 title "Nonlinear Structural Response in Flexible Flapping Wings with Different Density Ratio" @default.
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- W2321442237 doi "https://doi.org/10.2514/6.2011-376" @default.
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