Unsteady Simulation of a Synthetic Jet Actuator with Cylindrical Cavity Using a 3-D Lattice Boltzmann Method

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/9358132/figures/9358132.fig.004a.svgz" name="9358132.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Flux at the diaphragm and nozzle exit</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/9358132/figures/9358132.fig.004b.svgz" name="9358132.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Flux ratio at the diaphragm and nozzle exit</td></tr></table>

<div>Physical flux and flux ratio at the diaphragm and nozzle exit from 3rd working cycle to 5th working cycle.</div>

International Journal of Aerospace Engineering

fig4

Figure 4

Figure 4: Unsteady Simulation of a Synthetic Jet Actuator with Cylindrical Cavity Using a 3-D Lattice Boltzmann Method 