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- W4366128170 abstract "In this paper, the circular and non-circular twin jets are investigated numerically at two different spacing to diameter (S/D) ratios of 0.25 and 1.0, respectively. Here S is the spacing distance between the two individual jets, and D is the circular nozzle exit diameter, which is kept constant. Ellipse, Square, and Triangle plane twin jets are considered non-circular twin jets in the numerical investigation. The numerical simulations of twin jets are carried out at a transonic Mach number (M) of 0.8 using Reynolds-averaged Navier-Stokes (RANS) based two-equation Shear Stress Transport (SST) K-ω turbulence model. Comparison of the mean velocity profiles in the symmetry plane with experimental data indicates a good agreement. The results show that near the nozzle exit, the twin jets issuing into ambient conditions resembles a free jet, leading to a core length independent of spacing distance and similar to a free single round jet. The triangular single and twin jets are more effective in promoting the mixing characteristics in the jet near field over other non-circular jets." @default.
- W4366128170 created "2023-04-19" @default.
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- W4366128170 date "2023-01-01" @default.
- W4366128170 modified "2023-09-27" @default.
- W4366128170 title "Mixing Characteristics of Circular and Non-Circular Twin Jets at a Transonic Mach number 0.8" @default.
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- W4366128170 doi "https://doi.org/10.1007/978-981-19-6270-7_61" @default.
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