This study presents a geometric optimization of the Supersonic Molecular Beam Injection (SMBI) nozzle intended for the Thailand Tokamak-1 (TT-1), aiming to enhance fueling efficiency through improved particle penetration. Numerical simulations were performed using ANSYS Fluent, where hydrogen was used as the working fluid expanding from high-pressure stagnation conditions into the vacuum chamber. Variations in throat diameter, outlet diameter, divergent length, and inlet pressure were systematically investigated using a 2D axisymmetric computational domain and the SST k–ω turbulence model. The results show that the penetration depth strongly depends on the throat diameter, with an optimum value at 1.5 mm. The outlet diameter also plays a significant role, where a nozzle with equal inlet and outlet diameters of 6 mm achieved the maximum simulated penetration of approximately 6 mm. The divergent length exhibits only secondary influence compared with the throat and outlet sizes. Gas velocity increases substantially with increasing inlet pressure; however, excessively high pressures reduce cost-effectiveness. An inlet pressure of 0.5 MPa combined with a 24-mm divergent length is recommended as a practical compromise between performance and operational efficiency. The optimized geometry offers a credible design basis for the TT-1 SMBI system, and future work will involve fabrication and experimental validation during TT-1 plasma operations.
扫码关注我们
求助内容:
应助结果提醒方式:
