Open access
Sep 2026
Numerical and experimental study of tandem dual-jet injection into a supersonic cross-flow
Abstract Content of image described in text. To minimise the required length of supersonic-combustion ramjets (scramjets), injected fuel should mix rapidly with the supersonic cross-flow. Tandem dual-jet injection has shown improved mixing performance over single-jet injection. The present study comprises experimental...
J. Smink, E. V. D. van der Weide, S. de Maag et al.
· Journal of Fluid Mechanics · 0 citations