Time-Dependent Effects of Glaze Ice on the Aerodynamic Characteristics of an Airfoil

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijrm/volume-2018/2981739/figures/2981739.fig.0010a.svgz" name="2981739.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>One instant of negative lift</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijrm/volume-2018/2981739/figures/2981739.fig.0010b.svgz" name="2981739.fig.0010b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>One instant of positive lift</td></tr></table>

<div>Vortices shape at two moments with an interval of half period at zero angle of attack.</div>

International Journal of Rotating Machinery

fig10

Figure 10

Figure 10: Time-Dependent Effects of Glaze Ice on the Aerodynamic Characteristics of an Airfoil 