Experimental Study on the Aerodynamic Characteristics of Blades at the Last Stage of a Steam Turbine at Off-Design Conditions

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/8785963/figures/8785963.fig.006a.svgz" name="8785963.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Total pressure at L-0 inlet</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/8785963/figures/8785963.fig.006b.svgz" name="8785963.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Total pressure at L-0 outlet</td></tr></table>

<div>Total pressure distribution at L-0 inlet and outlet from TC2 to TC5.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Experimental Study on the Aerodynamic Characteristics of Blades at the Last Stage of a Steam Turbine at Off-Design Conditions 