Abstract A technique of analyzing the flutter initiation in flat plate compressor cascades was developed. The viscous and inviscid flow study was carried out using the COBRA solver based on the modified implicit Godunov method and unsteady implicit method updated for using. The flutter conditions were revealed and the effect of taking into account viscosity, angles of attack and time steps was investigated.
Analysis of flow past oscillating cascades by the implicit method to evaluate the cascade aeroelastic stability in viscous flow
Russian Aeronautics (Iz VUZ) ; 54 , 1 ; 9-14
2011-03-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Subsonic flow past an oscillating cascade with finite mean flow deflection
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