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In order to compare effectively the various loss correlations, all of the model results for the loss curves were shifted, or translated, on the loss versus incidence graphs so that the minimum-loss point of each correlation was positioned at the point of minimum-loss for the Rotor 1-B and Stage 35 experiments at a given corrected speed (see Figure 4.2). 0.14 0.14 Experimental Data Curve Predicted Data Curve 1 2 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 4.2 Translation of Model Results to Match Experimental Minimum-Loss Points Figure 4.2 depicts two loss curves, one being an experimental result and the other a data curve predicted using correlations. The minimum-loss point on the experimental result curve is labeled (1) and the minimum-loss point on the predicted curve is labeled (2). The entire predicted data curve is shifted, so that point (2) lies directly on top of point (1). This enables a qualitative analysis of the predicted curve as compared to the experimental curve. A similar method of transformation was used in evaluating the off- minimum-loss deviation angles. This time, however, the experimental deviation angle found at the minimum-loss point was used as the anchor for the off-minimum-loss deviation correlation curves. 33 Total Pressure Loss Coefficient( ω )PDF Image | Gas Turbine Design Axial Flow Compressors
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