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

Figure 4

Pressure and velocity-time histories at different axial locations (x/L = 0.25, 0.5, and 0.75): comparisons of analytical solution (dashed-dot) and numerical predictions using SIMPLE (solid) and PISO (dashed) algorithms at  = 1.0.

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