International Journal of Aerospace Engineering / 2012 / Article / Fig 11

Research Article

Multisized Inert Particle Loading for Solid Rocket Axial Combustion Instability Suppression

Figure 11

Predicted head-end pressure wave profile, reference motor (  s−1,  J/kg,  atm, %, μm, μm, μm, %, %, % ), three particle sets, acceleration active.

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