International Journal of Aerospace Engineering / 2012 / Article / Fig 4

Research Article

Multisized Inert Particle Loading for Solid Rocket Axial Combustion Instability Suppression

Figure 4

Predicted head-end pressure wave profile, reference motor (  s−1,  J/kg,  atm), acceleration nullified, 5% 10-μm Al particle loading by mass, single particle set.
173129.fig.004

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