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4.1 Data Reduction Methods Figure 4.1 depicts a loss curve for a transonic compressor using loss as the ordinate and incidence as the abscissa. Choke or Pressure Stall Side Suction Stall Side 0.12 0.12 0.1 0.1 0.08 0.08 0.06 0.04 0.04 0.02 0.02 00 -2 -1 0 1 2 3 4 5 6 Incidence (i) Minimum Loss Incidence (i*) Minimum Loss ωmin Figure 4.1 Division of Loss Curve into Choked and Stalled Regions The loss curve refers to the curve created by varying the flow incidence to the compressor blade and measuring the resulting non-dimensionalized total pressure loss coefficient as described in Section 2.2. The region to the right of the minimum-loss point where incidence is greater than the minimum-loss incidence is referred to as the stall regime because as the incidence is increased the trend on the suction side of the compressor blade is toward stalled flow. Moving in the direction to the left of the minimum-loss incidence, the flow will either choke or will separate from the pressure side of the compressor blade. This region is referred to as the choke regime. 32 Total Pressure Loss Coefficient( ω )PDF Image | Gas Turbine Design Axial Flow Compressors
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