A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left">Case</td><td class="align_center">Case 1</td><td class="align_center">Case 2</td><td class="align_center">Case 3</td><td class="align_center">Case 4</td><td class="align_center">Case 5</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">Combustion efficiency (%)</td><td class="align_center">57.393</td><td class="align_center">58.687</td><td class="align_center">59.531</td><td class="align_center">42.962</td><td class="align_center">67.164</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Combustion efficiency at the exit of the combustor.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor 