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Self-excited vibration of a palisade in 2D subsonic, transonic and supersonic flow

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In recent years coupled fluid-structure problems have appeared. The computational method used to solve this problem was based on a time-marching algorithm, so it was natural to consider a time domain flutter analysis method. The time domain method of flutter analysis is based on the simultaneous integration in time of the equation of motion for the structure and the fluid. The flow model is capable of representing 2D flows over a wide Mach number range from low subsonic to supersonic, including transonic flows. The aerodynamic model fully accounts for blade thickness and camber and the angle-of-attack effects. The unsteady Euler equations are integrated by using the explicit monotonous second-order accurate Godunov scheme. The blade is modelled on the basis of extended beam theory including a bending-bending-torsional vibration and also by the simple two-degree of freedom model. The equation of motion is obtained by using the extended Hamilton's principle and the Ritz method. The direct integration method is used to find a solution of the coupled fluid-structure problem. In this work the comparison of numerical and experimental results is presented for the first and fourth standard configurations.
Słowa kluczowe
EN
Rocznik
Strony
49--80
Opis fizyczny
Bibliogr. 22 poz., rys.
Twórcy
  • Institute cf Fluid-Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland
  • Polish Naval Academy, Faculty of Mechanical and Electrical Engineering, Gdynia, Poland
autor
  • Department of Hydromechanics of Power Machines, Institute for Problems in Machinery, Ukrainian National Academy of Sciences Pozarsky St. 2/10 Kharkov, 310046, Ukraine
Bibliografia
  • [1] Agnew R.P., Differential Equations, Mcgraw-Hill Company, Inc., 1960
  • [2] Arkadyev A.B., Gnesin V.I., Vanin V.A. and Yershov S.V., Unsteady Blade Forces Generated By Rotor-Stator Aerodynamic Interaction and Cascade Airfoils Oscillations, International Conference Engineering Aerohydroelasticity EAHA, December 5-8, Prague, Czech Republic, 1989,366
  • [3] Bakhale M.A., Reddy T.S.R. and Keith T.G., Time Domain Flutter Analysis of Cascade Using Full-Potential Solver, AIAA Journal, Vol. 30, No. 1, January 1992, 163
  • [4] Bathe K. and Wilson E., Numerical Methods in Finite Element Analysis, Prentice- Hall, Inc., Englewood Cliffs, New Jersey, 1976
  • [5] Bendiksen O.O., Role of Shock in Transonic/Supersonic Compressor Rotor Flutter, AIAA Journal, Vol. 24, No. 7, July 1986,1179
  • [6] Bisplinghoff R.L., Asley H. and Halfman R.L, Aeroelasticity, Addison-Wesley Publishing Company, Inc. Cambridge 42, Mass, 1955
  • [7] Boise A., and Fransson T.H., Aeroelasticity in Turbomachines Comparison of Theoretical and Experimental Cascade Results, Communication Du Laboratoire De Thermique Appliquee et Turbomachines, Nr. 13. Lusanne, Epfel, 1986
  • [8] Boise A., and Fransson T.H., Aeroelasticity in Turbomachines Comparison of Theoretical and Experimental Cascade Results, Communication Du Laboratoire De Thermique Appliquee et Turbomachines, Nr. 13, Appendix A5 All Experimental and Theoretical Results for The 9th Standard Configuration, Lusanne, Epfel, 1986
  • [9] Chmielniak T., Foundation of The Theory ofProfdes and Cascades, Part IV Ossolineum Polish Academy of Sciences, The Institute of Flow-Fluid Machinery, 1989 (in Polish)
  • [10] Eidelman S, Colella P. and Shreeve R., Application of The Godunov Method and Its Second-Order Extension To Cascade Flow Modeling, AIAA Journal, vol. 22, No. 11, 1984,1609
  • [11] Godunov, S.K. Et Al., Numerical Solution of Multidimensional Problem in Gas Dynamics, Nauka, Moscow, 1976 (in Russian)
  • [12] He L. and Denton J.D., Three Dimensional Time-Marching Inviscid and Viscous Solutions For Unsteady Flows Around Vibrating Blades, Asme Paper, 93-GT-92, 1993
  • [13] He L., Rotating-Stall/Stall-Flutter Prediction Using A Fluid/Structure Coupled Method, Proceedings of 7lh International Symposium On Unsteady Aerodynamics and Aeroelasticity of T urbomachines, September 25-29, Fukuoka, Japan, 1994,597
  • [14] Henry R. and Jacquet-Richardet G., Flutter Analysis in Blade Dynamics, 8th IFToMM World Congress, Theory of Machines and Mechanisms, Forced Vibrations of T urbomachine Blades, Prague, August 26-31,1991
  • [15] Hirsch C., Computation of Internal and External Flow, vol. 2 Computational Methods For Inviscid and Viscous Flows, John Wiley and Son, 1988
  • [16] Ramamurti V., Computer Aided Design in Mechanical Engineering, Tata Mcgraw-Hill Publishing Company Limited, New Delhi, 1989
  • [17] Rozhdestvenskij B.L. and Yanenko N.N., Systems of Quasilinear Equations and Their Applications To Gas Dynamics, 2nd. Ed., Nauka, Moscow (1978), Engl, transl., Transl. Math Monographs, vol. 55, Providence (1983), Zbl.513.35002, Zbl.177,140
  • [18] Rzqdkowski R., The General Model of Free Vibrations of Mis tuned B laded Discs. Part I. Theoretical Model. Part II. Numerical Results, Journal of Sound and Vibration, 173(3), 1994,395
  • [19] Rzqdkowski R., Dynamics of Steam Turbine Rotor Blading, Part II. B laded Discs, Ossolineum, Wroclaw, 1998
  • [20] Rzqdkowski R., Numerical Analysis of Free and Forced Vibration of Tuned and Mis tuned B laded Discs, Zeszyty Naukowe IMP PAN 483/1438/97 (PhD thesis)
  • [21] Rzqdkowski R., Gnesin V. and Kovalyov A., The 2D Flutter of Bladed Disc in An In- Compressible Flow, The 8th International Symposium of Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm, Sweden, September 14-18 1997
  • [22] Verdon J.K., Linearized Unsteady Aerodynamic Theory, AG ARD Manual On Aeroelasticity in Axial Flow Turbomachines, vol. 1, pp.(2-l, 2-31), 1987
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT3-0016-0063
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