Hybrid Numerical Simulation of Jet Blast Distance of a Departing Aircraft

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left">Internal nozzle static pressure (Pa)</td><td class="align_center">Internal nozzle static temperature (K)</td><td class="align_center">Mach number of internal nozzle</td><td class="align_center">External nozzle static pressure (Pa)</td><td class="align_center">External nozzle static temperature (K)</td><td class="align_center">Mach number of external nozzle</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">101325</td><td class="align_center">570</td><td class="align_center">0.8579</td><td class="align_center">101325</td><td class="align_center">328.15</td><td class="align_center">0.9045</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Dynamic boundary conditions of the A320 engine.</div>

Mathematical Problems in Engineering

tab4

Table 4

Table 4: Hybrid Numerical Simulation of Jet Blast Distance of a Departing Aircraft 