Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Acoustic mode</td><td class="align_center">1L</td><td class="align_center">2L</td><td class="align_center">1T</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Frequency (Hz)</td><td class="align_center">5280</td><td class="align_center">10560</td><td class="align_center">9773</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The theoretical characteristic frequencies of the chamber.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine 