A numerical study was conducted to explore the computational accuracy and efficiency of steady laminar flamelet model used in two-phase supersonic combustion flow field. The combustion flow field of a double-cavity scramjet was simulated. in which liquid phase was described by the disperse particle method (DPM) with secondary break-up process. The results obtained show that the steady... https://lecoureures.shop/product-category/ski-de-fond-accessoires-fartages/