Numerical Investigation of Combustion Characteristics of a Wave Rotor Combustor Based on a Reduced Reaction Mechanism of Ethylene

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Operating condition</td><td class="align_center">Species of hot-jet</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">Combustion products</td></tr><tr><td class="align_left">2</td><td class="align_center">N<sub>2</sub></td></tr><tr><td class="align_left">3</td><td class="align_center">Ar</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Parameters used to describe operating condition in simulation.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Numerical Investigation of Combustion Characteristics of a Wave Rotor Combustor Based on a Reduced Reaction Mechanism of Ethylene 