Stator clocking in SO3 compressor first stage rotor blades

• Autorzy: Rządkowski R , Gnesin V , Kolodyazhnaya L , Szczepanik R
• Konferencja: International Symposium SYMKOM Compressor & Turbine Flow Systems, Treory & Application Areas (15-17.09.2008; Łódź; Polska)
• Języki publikacji: EN

Abstrakty

EN

Numerical calculations of the 3D transonic flow of an ideal gas through three-row compressor stage including the clocking effects are presented. The approach is based on the solution of the coupled aerodynamic-structure problem for the 3D flow through the turbine stage in which fluid and dynamic equations are integrated simultaneously in time. There has been performed the calculation for the stage of the compressor with rotor blades of 0.163 m. The aeroelastic characteristics are obtained for different position of the stator rows. The clocking effect influence the stability region of the rotor blades.

Słowa kluczowe

EN

compressor; clocking; unsteady forces

PL

kompresor; siły nieustalone; obliczenia numeryczne

• Wydawca: Wydawnictwo Politechniki Łódzkiej
• Czasopismo: Zeszyty Naukowe. Cieplne Maszyny Przepływowe - Turbomachinery / Politechnika Łódzka
• Rocznik: 2008
• Tom: nr 133
• Strony: 299--308
• Opis fizyczny: Bibliogr. 23 poz.

Twórcy

autor

Rządkowski R

• Department of Dynamics of Machines, Institute of Fluid Flow Machinery, Polish Academy of Sciences, Gdansk

autor

Gnesin V

• Department of Aerohydromechanics, Institute for Problems in Machinery Ukrainian National Academy of Sciences, 2/10 Pozharsky st., Kharkov 310046

autor

Kolodyazhnaya L

• Department of Aerohydromechanics, Institute for Problems in Machinery Ukrainian National Academy of Sciences, 2/10 Pozharsky st., Kharkov 310046

autor

Szczepanik R

• Air Force Institute of Technology,Warszawa 01-494, Księcia Bolesława 46.

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