关键词:
Supersonic nozzle
Turbulence model
Numerical simulation
Performance analysis
摘要:
The nozzle is a critical component responsible for generating most of the net thrust in a scramjet *** quality of its design directly affects the performance of the entire propulsion ***,most turbulence models struggle to make accurate predictions for subsonic and supersonic flows in *** this study,we explored a novel model,the algebraic stress model k-kL-ARSM+J,to enhance the accuracy of turbulence numerical *** new model was used to conduct numerical simulations of the design and off-design performance of a 3D supersonic asymmetric truncated nozzle designed in our laboratory,with the aim of providing a realistic pattern of *** research indicates that,compared to linear eddy viscosity turbulence models such as k-kL and shear stress transport(SST),the k-kL-ARSM+J algebraic stress model shows better accuracy in predicting the performance of supersonic *** predictions were identical to the experimental values,enabling precise calculations of the *** performance trends of the nozzle are as follows:as the inlet Mach number increases,both thrust and pitching moment increase,but the rate of increase slows *** peaks near the design Mach number and then rapidly *** increasing inlet pressure,the nozzle thrust,lift,and pitching moment all show linear *** the flight altitude rises,the internal flow field within the nozzle remains relatively consistent due to the same supersonic nozzle inlet flow ***,external to the nozzle,the change in external flow pressure results in the nozzle exit transitioning from over-expanded to under-expanded,leading to a shear layer behind the nozzle that initially converges towards the nozzle center and then diverges.