Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing
This article presents the application of aeroelastic tailoring in the design of wings for a flying demonstrator, as well as the validation of the design methodology with flight test results.
Wolf R. Krüger +4 more
doaj +1 more source
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay
There is a strong aerodynamic interference when launching the missile in the embedded mode. During the separation process, the carrier aircraft safety may be threatened due to large slenderness ratio, low structural stiffness, and aeroelasticity effects ...
Shuling Tian, Rongjie Li, Ke Xu
doaj +1 more source
Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities [PDF]
A state feedback control law based on the sliding mode control method is derived for the aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer is constructed to estimate the unavailable state variables of the system.
Xingzhi Xu, Yakui Gao, Weiguo Zhang
openaire +3 more sources
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
doaj +1 more source
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
doaj +1 more source
On the validation and use of high-fidelity numerical simulations for gust response analysis [PDF]
Specific gust response is considered as one of the most important loads encountered by an aircraft. The Certification Specification (CS) 25, defined by the European Aviation Safety Agency (EASA), and the Federal Aviation Regulations (FAR) 25, defined by ...
Dequand, Sylvie +3 more
core +2 more sources
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
doaj +1 more source
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
doaj +1 more source
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
doaj +1 more source
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
doaj +1 more source

