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

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Overall parameter</td><td class="align_center">BWB-350</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Cruise altitude (m)</td><td class="align_center">11000</td></tr><tr><td class="align_left">Cruise Mach number (Ma)</td><td class="align_center">0.85</td></tr><tr><td class="align_left">Gliding speed (m/s)</td><td class="align_center">72</td></tr><tr><td class="align_left">Maximum takeoff weight (kg)</td><td class="align_center">230000</td></tr><tr><td class="align_left">Cruise lift-to-drag ratio (K)</td><td class="align_center">23</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Overall design parameters of BWB-350.</div>

International Journal of Aerospace Engineering

tab1

Table 1

Table 1: Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System 