On the Influence of the Mounting Stiffness on Dynamics of a Double-Link Aerodynamic Pendulum

 
PIIS086956520001373-3-1
DOI10.31857/S086956520001373-3
Publication type Article
Status Published
Authors
Occupation: leading researcher
Affiliation: Institute of Mechanics of Lomonosov MSU
Occupation: leading engineer
Affiliation: Institute of Mechanics of Lomonosov MSU
Journal nameDoklady Akademii nauk
Edition
Pages254-257
Abstract

Dynamics of a double aerodynamic pendulum is considered. The blade is rigidly attached to the second link. The first link of the pendulum is mounted elastically. The influence of the mounting stiffness upon the dynamics is analyzed. The conditions of stability are derived for the steady state of the system in which both links are directed along the flow. It is shown that the increasing of the mounting stiffness can lead to the loss of stability of this steady state. Experiments with such pendulum were performed in the wind tunnel of the Institute of Mechanics of Lomonosov MSU. The speed of the flow and the locations of the blade with respect to the second link were varied. The experimental data are in the qualitative agreement with the results of numerical simulation.

Keywordsself-sustained oscillations, aeroelasticity, limit cycles, wind power station, stability
Received14.10.2018
Publication date16.10.2018
Number of characters552
Cite   Download pdf To download PDF you should sign in
Размещенный ниже текст является ознакомительной версией и может не соответствовать печатной

views: 1310

Readers community rating: votes 0

1. Abdelkefi A. Aeroelastic energy harvesting. A review. // Int. J. Engineering Science. 2016. Vol. 100. P. 112–135.

2. Klimina L., Dosaev M., Selyutskiy Yu. Asymptotic analysis of the mathematical model of a wind-powered vehicle // Applied Mathematical Modelling. Elsevier BV. 2017. Vol. 46. P. 691–697.

3. Strganac T.W., Ko J., Kurdila A.J. Identification and Control of Limit Cycle Oscillations in Aeroelastic Systems // Journal of Guidance, Control, and Dynamics. 2000. Vol. 23, N 6. P. 1127–1133.

4. Dimitriadis G., Li J. Bifurcation behavior of airfoil undergoing stall flutter oscillations in low-speed wind tunnel // AIAA Journal. 2009. Vol. 47, N 11. P. 2577–2596.

5. Amandolese X., Michelin S., Choquel M. Low speed flutter and limit cycle oscillations of a two–degree of freedom flat plate in a wind tunnel // J. of Fluids and Structures. 2013. Vol. 43. P. 244–255.

6. Vitaly A. Samsonov, Marat Z. Dosaev, Yury D. Selyutskiy. Methods of qualitative analysis in the problem of rigid body motion in medium. // Int. J. Bifurcation and Chaos. 2011. Vol. 21, N 10. P. 2955–2961.

7. Holub A.P., Selyutskiy Y.D. On the influence of elastic fastening on the oscillations of a two-link aerodynamic pendulum // Proceedings of Moscow Institute for Physics and Technology. 2017. N 3. P. 8 – 13.

8. Sheldahl R.E., Klimas, P.C. Aerodynamic Characteristics of Seven Symmetrical Airfoil sections Through 180 Degree Angle of Attack for Use in Aerodynamic Analysis of Vertical Axis Wind Turbines // Sandia National Laboratories: Albuquerque. 1981. P. 118.

Система Orphus

Loading...
Up