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Gas Turbine NOx Water & Steam Injection Calculator engineering
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Gas Turbine NOx Water & Steam Injection Calculator

Compute thermal NOx suppression, water-to-fuel injection ratio (Ω), heat rate penalty, and mass flow power boost in heavy-duty gas turbines.

Combustor & Fuel Parameters

Injection Ratio & Cycle Performance

Water/Fuel Mass Ratio (Ω):
Injection Fluid Flow Rate:
Mass Power Boost (ΔP_shaft):
Heat Rate Penalty:
Combustor Flame Peak Temp:
NOx Reduction Percentage:

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Thermal NOx & Zeldovich Kinetics

Thermal nitrogen oxides ($NO_x$) form via the extended Zeldovich mechanism when atmospheric nitrogen and oxygen react in combustor primary flame zones above $1500^\circ\text{C}$ ($2800^\circ\text{F}$). The formation rate escalates exponentially with peak stoichiometric flame temperature.

Water vs Steam Injection Mechanisms

Injecting demineralized water directly into the fuel nozzle acts as a thermal heat sink. As liquid water droplets absorb latent heat of vaporization ($h_{fg} \approx 2257\text{ kJ/kg}$) and sensible heat, flame temperature is quenched by $150^\circ\text{C}$ to $250^\circ\text{C}$, cutting $NO_x$ by up to $85\%$. Injected mass expands across the turbine section, creating a temporary peak power boost at the expense of cycle thermal efficiency.

Frequently Asked Questions