4.6 Review

A review of membrane-wing aeroelasticity

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Eigenmode analysis of membrane stability in inviscid flow

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Summary: The study investigates the instability of a thin membrane immersed in an inviscid fluid flow, shedding a trailing vortex-sheet wake. By solving the nonlinear eigenvalue problem with various initial guesses under three canonical boundary conditions and over a wide range of mass densities, the researchers observe instability by divergence or flutter, particularly at large mass density or with free ends. The most unstable eigenmodes become wavier at smaller mass density and tension, showing nonmonotonic behavior in certain regions. While there is good quantitative agreement with unsteady time-stepping simulations at small amplitudes, only qualitative similarities are found with the eventual steady-state large-amplitude motions.

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Camber and aerodynamic performance of compliant membrane wings

Rye M. Waldman et al.

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Electro-aeromechanical modelling of actuated membrane wings

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Justin W. Jaworski et al.

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Aerodynamic Characterization of a Wing Membrane with Variable Compliance

Oscar M. Curet et al.

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Raymond E. Gordnier et al.

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Control of low Reynolds number flows by means of fluid-structure interactions

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Sara Arbos-Torrent et al.

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Thomas J. Mueller

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Aeromechanics of membrane wings with implications for animal flight

Arnold Song et al.

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Detached-Eddy Simulation

Philippe R. Spalart

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Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

Bret Stanford et al.

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Leading-edge vortex improves lift in slow-flying bats

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Static aeroelastic model validation of membrane micro air vehicle wings

Bret Stanford et al.

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Y. Elimelech et al.

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Laminar-turbulent transition of a low Reynolds number rigid or flexible airfoil

Yongsheng Lian et al.

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Stability of membrane in low subsonic flow

Ryszard Sygulski

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Challenges facing future micro-air-vehicle development

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S Miranda et al.

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YS Lian et al.

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Development of a three-dimensional viscous aeroelastic solver for nonlinear panel flutter

RE Gordnier et al.

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Structural optimization using computational aerodynamics

DE Raveh et al.

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