Tytuł artykułu
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Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Konferencja
International Symposium on Compressor and Turbine Flow Systems - Theory and Application Areas "SYMKOM" (10 ; 26-28.10.2011 ; Łódź, Polska)
Języki publikacji
Abstrakty
In this study numerical simulations of 2D viscous flutter were performed and compared with available experimental results for various mesh densities and flow parameters. Calculations were carried out for the bending oscillations of an Eleventh Standard Configuration cascade. ANSYS CFX code was used for the SST, SA and k-ω turbulence model calculations.
Słowa kluczowe
Rocznik
Tom
Strony
169--178
Opis fizyczny
Bibliogr. 9 poz.
Twórcy
autor
autor
autor
- Institute of Fluid Flow Machinery, Polish Academy of Sciences, Gdańsk, apajak@imp.gda.pl
Bibliografia
- [1] Chassaing J.C. and Gerolymos G.A., 2001, Compressor Flutter Analysis Using Time Nonlinear and Time Linearized 3D Navier-Stokes Method, in book P. Farrand, S. Auber: Unsteady Aerodynamics, Aeroacustics and Aeroelaslicity of Turbomachines, Proceedings of the 9th International Symposium held in Lyon, France, 4-8 September 2000, Presses Universitaires de Grenoble, 666-677.
- [2] Cinnella P., Palma P. De., Pascazio G., Napolitano, M., A Numerical Method for Turbomachinery Aeroelasticity, Journal of Turbomachinery, 2004, Vol. 126, 310-316.
- [3] Fransson T.H., Jocker M., Bolcs A., Ott P., Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi-3D Experimental Data for a New Aeroelastic Turbine Standard Configuration, Journal of Turbomachinery, 1999. Vol. 121, No. 4, 717-725.
- [4] Marshall J.G. and Imregun M., A Review of Aeroelasticity Methods with Emphasis on Turbomachinery Applications, Journal of Fluids and Structures, 1996, Vol. 10, 237-257.
- [5] McBean I., Liu F., Hourigan K., Thompson, M., Simulation of Aeroelasticity in an Annular Cascade using a Parallel 3-Dimensional Navier-Stokes Solver, 2002, Proceedings of ASME Turbo Expo 2002, Amsterdam, GT-2002-30366.
- [6] Rzadkowski R., Gnesin V., Kolodyazhnaya L., 3D Viscous Flutter of 11th Configuration Blade Row, Advances in Vibration Engineering, 2009, 8(3), 213-228.
- [7] Sayma A.I., Vahdati M., Green J.S., Irnregun M., 1998, Whote-Assembly Flutter Analysis of a Low Pressure Turbine Blade, in book T.H. Fransson ed.: Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Proceedings of the 8th International Symposium held in Stockholm, Sweden, 14-18 September 1997, Kluwer Academic Publishers, 347-359.
- [8] Vasanthakumar P., Chen T., He L., 2001, Three-Dimensional Viscous Computation of Blade Flutter and Forced Response Using Nonlinear Harmonic Approach, in book P. Farrand, S. Auber: Unsteady Aerodynamics, Aeroacustics and Aeroelasticity of Turbomachines, Proceedings of the 9th International Symposium held in Lyon, France, 4-8 September 2000, Presses Universitaires de Grenoble, 649-665.
- [9] 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 book T.H. Fransson ed.; Unsteady Aerodynamics and Aeroelasticily of Turbomachines, Proceedings of the 8th International Symposium held in Stockholm, Sweden, 14-18 September 1997, Kluwer Academic Publishers, 478-491.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD9-0028-0026