Meaning
Pressure comparison metrics dividing total gas stagnation pressure upstream of a convergent-divergent passage by static ambient pressure downstream establish the gas expansion regime in atomization nozzles. In powder metallurgy for battery alloy production, nozzle pressure ratio dictates whether gas flow reaches supersonic velocities needed for droplet shearing. The dimensioned ratio governs gas velocity and shock structure at the melt exit.
Its governing boundary ends at the nozzle exit plane where shock wave interactions dissipate into ambient gas.
Flow Thermodynamics
Gas expansion efficiency through a nozzle depends on the pressure differential maintained across the throat. When operating at a high nozzle pressure ratio, gas accelerates past choked flow conditions to achieve Mach numbers exceeding unity. This mechanical compression ratio determines the acoustic wave structure formed within the exit cone.
Insufficient pressure differential causes flow separation inside the nozzle divergent section, reducing kinetic energy transfer to the molten metal stream.
Expansion Behavior
Underexpanded and overexpanded gas jets alter the atomization gas plume geometry, affecting droplet cooling rates and powder uniformity. Adjusting nozzle pressure ratio changes the position of shock diamonds downstream of the nozzle exit plane. When the ratio matches design conditions, shock-free expansion delivers maximum momentum to the liquid melt interface.
Deviations from design values increase gas consumption without improving powder fineness.
Velocity Boundary
Supersonic gas flow terminates as shock structures interact with ambient chamber atmospheres downstream. Once gas exits the nozzle near field, nozzle pressure ratio no longer dictates local flow acceleration or droplet shearing forces.