Results 11 to 20 of about 11,119 (215)
NUMERICAL APPROACH IN AEROELASTICITY [PDF]
Aircraft wing design processes should comprise specific analyses oriented towards aeroelasticity, which is one of the essential factors determining flight envelope boundaries.
Oskar SLOBODA +3 more
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Viscoelastic damping design – Thermal impact on a constrained layer damping treatment
Constrained layer damping treatments have been commonly used for vibration damping. The included viscoelastic material exhibits high damping potential that is retrieved under shear deformation.
Martin Gröhlich +3 more
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Design and Optimization of an Aeroservoelastic Wind Tunnel Model
Through the combination of passive and active load alleviation techniques, this paper presents the design, optimization, manufacturing, and update of a flexible composite wind tunnel model.
Johannes K. S. Dillinger +4 more
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NUMERICAL SIMULATION OF OSCILLATIONS OF A PLATE IN RESTING FLUID
This paper presents a numerical solution of the problem of oscillations of a flexible plate placed in a viscous incompressible fluid done with ANSYS. In constructing a finite element model of the plate, both volumetric and shell finite elements, which ...
Irina Negrozova, Oleg Goryachevsky
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Modeling and Analysis of Aeroelasticity and Sloshing for Liquid Rocket
In this paper, based on the advantages of Newtonian mechanics method, mixed coordinate method, and analytical mechanics method, the dynamic model of rigid-aeroelasticity-sloshing coupling is established for longitudinal vibration and liquid fuel sloshing,
Dewei Zhang +4 more
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Aerodynamic Performance and Wake Flow of Crosswind Kite Power Systems
This paper presents some results from a computational fluid dynamics (CFD) model of a multi-megawatt crosswind kite spinning on a circular path in a straight downwind configuration. The unsteady Reynolds averaged Navier-Stokes equations closed by the k−ω
Mojtaba Kheiri +4 more
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Measurement of FRFs and Modal Identification in Case of Correlated Multi-Point Excitation
The modal identification of large and dynamically complex structures often requires a multi-point excitation. Sine sweep excitation runs are applied when it is necessary to concentrate more energy on each line of the frequency spectrum.
U. Fuellekrug +3 more
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Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing
A composite high-aspect-ratio wing of a high-altitude long-endurance (HALE) aircraft was modeled with FEM by MSC/NASTRAN, and the nonlinear static equilibrium state is calculated under design load with follower force effect, but without load ...
Chang Chuan Xie +2 more
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Numerical Simulations on Unsteady Nonlinear Transonic Airfoil Flow
Large-amplitude excitations need to be considered for gust load analyses of transport aircraft in cruise flight conditions. Nonlinear amplitude effects in transonic flow are, however, only marginally taken into account.
Diliana Friedewald
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This chapter deals with the basic principles of aeroelasticity theory (Theodorsen theory) and how these can be applied to bridge structures with sensitive deck shapes. The most common aerodynamical models with two or three forces as well as buffeting forces are briefly presented.
openaire +2 more sources

