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

<table class="table-group" id="tab3"><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_left"></td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Axial length of fan section (m)</td><td class="align_center">1.08</td></tr><tr><td class="align_left">Maximum outer diameter of engine (m)</td><td class="align_center">1.964</td></tr><tr><td class="align_left">Inner diameter of engine (m)</td><td class="align_center">0.9</td></tr><tr><td class="align_left">Number of fan stages</td><td class="align_center">1</td></tr><tr><td class="align_left">Rotor–stator ratio</td><td class="align_center">1 : 2</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Distributed power system parameters of BWB-350.</div>

International Journal of Aerospace Engineering

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Table 3

Table 3: Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System 