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Experimental investigation of palisade flutter for the harmonic oscillations

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
PL
Eksperymentalne badania drgań opalowania w wibracjach harmonicznych
Języki publikacji
EN
Abstrakty
EN
The experimental stand for the flutter analysis was described. In this stand one can measure simultaneously unsteady aerodynamic force and moment with arbitrary combinations of bending and torsion motions of airfoil cascades in the subsonic flow. The cascade is composed of nine blades, four of them are vibrating. Unsteady flow effects have been investigated for subsonic flow in a compressor cascade. Specifically, experimental forced bending and torsion vibration were performed. The aerodynamic work coefficient of bending and torsional cascade vibrations for different interblade phase angles, Strouhal Numbers, and the incidence angles were shown.
Słowa kluczowe
Rocznik
Tom
Strony
3--26
Opis fizyczny
Bibliogr. 19 poz., rys., tab.
Twórcy
  • Institute for Prob]ems of Strength of the Nationa| Academy of Sciences of [Jktaine, Timirjazivska St. 2, 01014 Kyiv, Ukraine
  • Institute for Prob]ems of Strength of the Nationa| Academy of Sciences of [Jktaine, Timirjazivska St. 2, 01014 Kyiv, Ukraine
  • The Szewalski Institute of Fluid-Flow Machinery, Polish Academy of Sciences, Fiszera 74, 80-952 Gdańsk, Poland
Bibliografia
  • [1] Stel’makh A.L., Kaminer A.A.: Effect of the geometrical parameters of a compressor cascade on the limit of bending self-oscillations of blades caused by cascade flutter, Strength of Materials, 15(1983), No. 1, 104-109.
  • [2] Kaminer A.A., Stel’makh A.L.: Effect of the aerodynamic connectedless between blades of the aerodynamic damping of their vibrations, and origin of cascade flutter, Strength of Materials, 14(1996), No. 12, 1667-1672.
  • [3] Len A.D., Kaminer A.A., Stel’makh A.L., Balalaev V.A.: Loss of dynamic stability of torsional vibrations of blades due to cascade flutter, Strength of Materials, 18(1986), No.1, 76-80.
  • [4] Stel’makh A. L.: Aerodamping and stability of compressor cascades in laminar and stall conditions, Vibrations in Technics and Technologies, 1999, No. 1(10), 45-51 (in Russian).
  • [5] A. Bolcs, T.H. Fransson (Eds.): Aeroelasticity in turbomachines: Comparison of theoretical and experimental cascade results, Comm. du Labor. de Therm. Appliq. et de Turbomachines, Lausanne, EPFL, N 13, 1986, p. 230.
  • [6] Gnesin V., Rządkowski R.: The theoretical model of 3D flutter in subsonic, transonic and supersonic inviscid flow, Trans. IFFM, No. 106, 2000, 45-68.
  • [7] Rządkowski R., Gnesin V.: The numerical and experimantal verification of the 3D inviscid code, Trans. IFFM, No. 106, 2000, 69-95.
  • [8] Gnesin V., Kolodyazhnaya L, Rządkowski R: Coupled aeroelastic oscillations of a turbine blade row in 3D transonic flow, J. of Thermal Sci., Vol. 10, 2001, No. 4, 318-324.
  • [9] Gnesin V., Rządkowski R., Kolodyazhnaya L.: A coupled fluid-structure analysis for 3D flutter in turbomachines, ASME Paper, No 2000-GT-380, 2000.
  • [10] Slater J.C., Minkiewicz G.R., Blair A.J.: Forced response of bladed disk assemblies – A survey, The Shock and Vibr. Digest, 31(1999), 17-24.
  • [11] Caminer A.A., Nastenko N.Ya.: Method for studying aerodynamic damping of turbomachine blades vibrations in air flows at various modes of vibration, [in:] Energy Dissip. During Vibration of Mechanical Systems, Kyiv, Naukova Dumka, 1973, 298-304 (in Russian).
  • [12] Kurzin V.B., Korostelev A.E.: Experimental determination of unsteady aerodynamic characteristics of an airfoil cascade, Energomashinostroenye, No. 1, 1974, 22-24 (in Russian).
  • [13] Karta D., Hiler T.: The experimental analysis of stability parameters of vibrating cascade in stall transonic flow, Energetycheske Mashiny i Ustanovky, No. 1(1978), 128-139 (in Russian).
  • [14] Tanaka H., Fujimoto I., Ishii S.: Aerodynamic response of a blade in pitching oscillation with partial and full separation, Novosti Zarubezhnoi Nauki i Tekhniki, 8, 1984, 25-28 (in Russian).
  • [15] Whitehead D. Watson P. et al.: The experiment for measurement moment coefficient of the vibrating cascade, Mir, 1979, 166-177 (in Russian).
  • [16] Kimura H., Nomiyama A.: An Experimental Study of Unsteady Aerodynamic Forces an a Rectangular Wing Oscillating in Pitch at Mach Numbers from 0.38 to 1.28, Memoirs of the Faculty of Eng. Kyushu Univ., 1977, 37, 3, 157-174.
  • [17] Kaminer A.A., Chervonenko A.G., Tsymbalyuk V.A.: Method for studying unsteady aerodynamic characteristics of airfoil cascades vibrating in a three-dimensional flow, Preprint Inst. for Problems of Strength, Acad. Sci. of the USSR, Kyiv 1988 (in Russian).
  • [18] Tsimbalyuk V.A.: Method of measuring transient aerodynamic forces and moments on vibrating cascade, Strength of Materials, 28(1996), No. 2, 150-157.
  • [19] Rządkowski R.: Dynamics of Rotor Steam Turbine Blading, Part Two, Bladed Discs, Fluid-Flow Machinery Series, Vol. 22, Ossolineum, Wrocław 1998.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWM2-0039-0036
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