Investigation of Flow Control for the Hypersonic Inlets via Counter Flow

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/956317/figures/956317.fig.001a.svgz" name="956317.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Started flow field</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/956317/figures/956317.fig.001b.svgz" name="956317.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Unstarted flow field</td></tr></table>

<div>Schlieren visualisation of an interaction between the forebody waves and the lip boundary layer in the hypersonic inlets.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Investigation of Flow Control for the Hypersonic Inlets via Counter Flow 