Numerical analysis investigates interactions between supersonic nozzle exit flows, suggesting interference across distances.
This study focuses on the numerical analysis of the interaction between the exit flows of two supersonic nozzles, using the distance between their longitudinal axes as a parameter. The analysis is conducted in OpenFOAM, assuming two-dimensional, inviscid flow. The methodology employed to simulate flow in a nozzle is validated against experimental data and is subsequently used to investigate the interaction with a second nozzle. The numerical results indicate that discharge flows interfere, even from distant nozzles.
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Mamaní et al. (2025) studied this question.
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