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

<div>Comparison between the computational and analytical results for the pressure-time history at the midlength of the chamber, <i>ε</i> = 0.1 and <i>ω</i> = 1.0 (<i>f</i>′ = 159 Hz).</div>

Mathematical Problems in Engineering

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Figure 3

Figure 3: Turbulent Flow Characteristics in a Model of a Solid Rocket Motor Chamber with Sidewall Mass Injection and End-Wall Disturbance 