Simplified theoretical formulae for the calculation of the axial and the transversal speeds of open-jet flow were presented. And the effects of two control parameters
ie
the offset parameter and the spreading rate
on the speed profile were analyzed. Experimental studies were performed in two wind tunnels respectively. The distributions of shear-layer speed profile
shear-layer thickness
turbulence intensity and turbulence spectrum were obtained. And the obtained data were compared with theoretical predictions. Results indicated that: beyond a distance from the nozzle
the axial speed profile was strongly self-similar
while the transversal speed profile was weakly self-similar; the shear-layer thickness linearly increased with stream-wise distance; the turbulence intensity was small and stable in the core flow region
slowly but linearly increased in the fully developed region
and rapidly increased in the shear-layer region; the shear-layer turbulence spectrum was broadband