Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="8"><hr/></td></tr><tr class="thead"><td class="align_left">Experiment</td><td class="align_center">A-1</td><td class="align_center">A-2</td><td class="align_center">A-3</td><td class="align_center">A-4</td><td class="align_center">Average temperature/K</td><td class="align_center">Case 2 calculation temperature/K</td><td class="align_center">Deviation</td></tr><tr><td class="thead-hr" colspan="8"><hr/></td></tr><tr><td class="align_left">Temperature/K</td><td class="align_center">671</td><td class="align_center">594</td><td class="align_center">565</td><td class="align_center">707</td><td class="align_center">634.3</td><td class="align_center">602</td><td class="align_center">5.36%</td></tr><tr class="table-tr"><td colspan="8"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison of temperature at point 1 for the simulation and experiments.</div>

International Journal of Aerospace Engineering

tab2

Table 2

Table 2: Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet 