Numerical Investigation of the Trailing Edge Shape on the Added Damping of a Kaplan Turbine Runner

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">(Hz)</td><td class="align_center">Frequency interactives</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Initial frq.</td><td class="align_center">189.94</td></tr><tr><td class="align_left">Step 1</td><td class="align_center">191.26</td></tr><tr><td class="align_left">Step 2</td><td class="align_center">191.41</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr><tr class="table-fn"><td><div>The final damping ratios of the blunt and Donaldson hydrofoil under different inlet velocities have been shown in Figures <a href="../fig10/#a">10(a)</a> and <a href="../fig10/#b">10(b)</a>, respectively.<br/></div></td></tr></table>

Mathematical Problems in Engineering

tab2

Table 2

Table 2: Numerical Investigation of the Trailing Edge Shape on the Added Damping of a Kaplan Turbine Runner 