where U is the phase-averaged
axial jet velocity at the nozzle exit plane, T is the period, and An is the nozzle exit area.
This method, based on mass and momentum conservation laws, has been extensively discussed (see, e.g., [2-4]) and is in good agreement with experiments except far away from the jet center part where it overestimates the
axial jet velocity field [1, 2].
While at Rolls-Royce, Griffith proposed the A J65
axial jet, with 6,500lb thrust, which led to the Avon.
Quadro's Ytron Jet Mixer uses a specially desiged impellor/stator to deliver a pure
axial jet flow, preventing vortices, unwanted air, and generating the efficient mixing that revolutionizes your process without the need for baffles in the vessel.