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3D model of viscous flutter of turbine rotor blades

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this study, numerical simulations of 3D viscous flutter were performed and compared with the available experimental results. The calculations were carried out for bending oscillations or the cascade known as the Eleventh Standard Configuration. The developed numerical algorithm solves 3D Reynolds-averaged Navier-Stokes equation together with the Baldwin-Lomax, using the explicit monotonous second-order accurate Godunov-Kolgan finite-volume scheme and moving hybrid H-O structured grid. Comparison of the calculated and experimental results for the Eleventh Standard Configurations has shown good quantitative and qualitative agreement for local performances (unsteady pressure amplitude and phase distribution) at off-design conditions. Benchmark solutions are provided for various values of the inter-blade phase angle O, 180, -90, 90, 72, -72 deg.
Słowa kluczowe
Rocznik
Tom
Strony
3--22
Opis fizyczny
Bibliogr.8 poz., rys.
Twórcy
autor
  • The Szewalski lnstitute of Fluid Flow Machinery, Department of Dynamics of Machines, Polish Academy of Sciences, Gdańsk, Poland, z3@imp.gda.pl
Bibliografia
  • [1] Marshall, J.G. and Imregun M.: A review of aeroelasticity methods with emphasis on turbomachinery applications, J. of Fluids and Structures, Vol. 10, 237-257, 1996.
  • [2] Sayma A.I., Validati M., Green J.S. Imregun M.: Whole - assembly flutter analysis of a low pressure turbine blade, [in:] T.H. Fransson ed., Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Proc. of the 8th Int. Symp. held in Stockholm, Sweden, 14-18 September 1997, Kluwer Academic Publ., 1998, 347-359.
  • [3] Weber S., Gallus H.E., Peitsch D.: 1998, Numerical solution of the Navier-Stokes equations for unsteady unstalled and stalled flow in turbomachniery cascade with oscillating blades, [in:] T.H. Fransson ed.: Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Proc. of the 8th Inter. Symp. held in Stockholm, Sweden, 14-18 September 1997, Kluwer Academic Publishers, 1998478-491.
  • [4] Vasanthakvunar P., Chen T., He L.: Three-dimensional viscous computation of blade flutter and forced response using nonlinear harmonic approach, [in:] P. Farrand, S. Auber : Unsteady Aerodynamics, Aeroacustics and Aeroelasticity of Turbomachines, Proc. of the 9th Inter. Symp. held in Lyon, France, 4-8 September 2000, Presses Universitaires de Grenoble, 2001, 649-665.
  • [5] Chassaing J.C, Gerolymos G.A.: 2001, Compressor flutter analysis using time-nonlinear and time-linearized 3-D Navier-Stokes method, [in:] P. Farrand, S. Auber: Unsteady Aerodynamics, Aeroacustics and Aeroelasticity of Turbomachines, Proc. of the 9th Inter. Symp. held in Lyon, France, 4- 8 September 2000, Presses Universitaires de Grenoble, 2001, 666-677.
  • [6] McBean I., Liu F., Hourigan K., Thompson M.: Simulation of aeroelasticity in an annular cascade using a parallel 3-dimensional Navier-Stokes solver, Proc. of ASME Turbo Expo 2002, June 2-6, 2002, Amsterdam, 2002, GT- 2002-30366.
  • [7] Fransson T.H., Jocker M., A. Boles, P. Ott: Viscous and inviscid linear/nonlinear calculations versus quasi-three-dimensional experimental data for a new aeroelastic turbine standard configuration, ASME J. of Turboma- chinery, Vol. 121, 1999, 717-725.
  • [8] Cinnella P., Palma P.De., Pascazio G., Napolitano M.: A Numerical method for turbomachinery aeroelasticity, J. of Turbomachinery, Vol. 126, April 2004, 310-316.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWM4-0008-0014
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