Hybrid Numerical Simulation of Jet Blast Distance of a Departing Aircraft

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Maximum take-off thrust (daN)</td><td class="align_center">Air mass flow (kg/s)</td><td class="align_center">Bypass ratio</td><td class="align_center">Diameter (mm)</td><td class="align_center">Engine outlet temperature (°C)</td></tr><tr><td class="align_left">13360</td><td class="align_center">390.5</td><td class="align_center">5.0</td><td class="align_center">1735</td><td class="align_center">297</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

tab3

Table 3

Table 3: Hybrid Numerical Simulation of Jet Blast Distance of a Departing Aircraft 