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

<table class="table-group" id="tab9"><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">Total inlet temperature (K)</td><td class="align_center">294</td></tr><tr><td class="align_left">Total inlet pressure (Pa)</td><td class="align_center">104365</td></tr><tr><td class="align_left">Inlet Mach number (Ma)</td><td class="align_center">0.25</td></tr><tr><td class="align_left">Static outlet pressure (Pa)</td><td class="align_center">101325</td></tr><tr><td class="align_left">Reynolds number</td><td class="align_center">700000</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Internal flow grid verification calculation conditions.</div>

International Journal of Aerospace Engineering

tab9

Table 9

Table 9: Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System 