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- W4281557524 abstract "An efficient and reliable stall inception prediction model is established and integrated into the compressor design. And the effect of blade loading distribution on flow stability of axial compressor is studied via the proposed method. Foreloaded, aft-loaded and uniformly loaded rotor blades of a subsonic axial compressor are designed by modifying the circulation distribution at the blade region during through-flow calculation. The design criterion is to keep the compressor characteristics unchanged at the design point. The steady numerical simulations of these cases show that the static pressure rise coefficient and adiabatic efficiency of the compressor with aft-loaded rotor blades are the best at small mass flow points, while those for fore-loaded rotor blades are the worst. The flow stability analysis of these cases via the developed model indicates that the compressor with aft-loaded rotor blades has the best stall margin, while that of the compressor with fore-loaded rotor blades is the worst. The steady flow fields are analyzed to reveal the effect mechanism, and the analysis confirms the above conclusion." @default.
- W4281557524 created "2022-05-27" @default.
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- W4281557524 date "2022-04-12" @default.
- W4281557524 modified "2023-09-26" @default.
- W4281557524 title "Effect of Blade Loading Distribution on Flow Stability of Axial Compressor" @default.
- W4281557524 doi "https://doi.org/10.33737/gpps21-tc-364" @default.
- W4281557524 hasPublicationYear "2022" @default.
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