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

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Pressure (MPa)</td><td class="align_center">Temperature (K)</td><td class="align_center">Velocity (m/s)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">1.5</td><td class="align_center">650</td><td class="align_center">762</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

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Table 4

Table 4: A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor 