Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5128136/figures/5128136.fig.0011a.svgz" name="5128136.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift coefficient comparison</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5128136/figures/5128136.fig.0011b.svgz" name="5128136.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Drag coefficient comparison</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5128136/figures/5128136.fig.0011c.svgz" name="5128136.fig.0011c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Lift-to-drag ratio comparison</td></tr></table>

<div>Calculation results of original boundary conditions and coupling point boundary conditions.</div>

International Journal of Aerospace Engineering

fig11

Figure 11

Figure 11: Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System 