Turbulent Flow Characteristics in a Model of a Solid Rocket Motor Chamber with Sidewall Mass Injection and End-Wall Disturbance

<div>Comparison between the experimental and computational results for the pressure-time history at (<i>x</i>) = 0.125, <i>ε</i> = 0.045, and <i>ω</i> = 0.52 (<i>f</i>′ = 63.44 Hz).</div>

Mathematical Problems in Engineering

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Figure 2

Figure 2: Turbulent Flow Characteristics in a Model of a Solid Rocket Motor Chamber with Sidewall Mass Injection and End-Wall Disturbance 