Inzynieria Chemiczna i Procesowa, Vol.27, No.3, 985-997, 2006
Experimental and numerical analysis of a streamwise vortex generator for subsonic flow
The total pressure measurements at two sections downstream of the jet hole (streamwise vortex generator) for the main flow Mach numbers 0.3 and 0.8 are presented. Experimental data are compared with the numerical results (FLUENT and SPARC) for one jet hole inclination. Differences of the streamwise vortex structures predicted by the codes are compared.