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

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Overall parameters</td><td class="align_center">Design values</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Blade chord length (m)</td><td class="align_center">0.1273</td></tr><tr><td class="align_left">Leading edge radius (m)</td><td class="align_center">0.00114</td></tr><tr><td class="align_left">Trailing edge radius (m)</td><td class="align_center">0.00157</td></tr><tr><td class="align_left">Installation angle (°)</td><td class="align_center">14.2</td></tr><tr><td class="align_left">Trailing angle (°)</td><td class="align_center">14.4</td></tr><tr><td class="align_left">Grid distance (m)</td><td class="align_center">0.254</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System 