International Journal of Aerospace Engineering / 2012 / Article / Fig 9

Research Article

Multisized Inert Particle Loading for Solid Rocket Axial Combustion Instability Suppression

Figure 9

Predicted head-end pressure wave profile, reference motor (  s−1,  J/kg,  atm, %, μm, μm, μm, %, %, α p3 = 0.5% ), three particle sets, acceleration active.
173129.fig.009

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