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Gas Air Systems

Reference data and engineering information about gas air systems for combustion applications.

gasairsystems

Overview

Engineering reference data for Gas Air Systems in combustion engineering.

Key Formulas

Heat Release

Q=m˙HVQ = \dot{m} \cdot HV

Fuel energy release rate.

Air-Fuel Ratio

AF=mairmfuelAF = \frac{m_{air}}{m_{fuel}}

Mass of air per mass of fuel.

Excess Air

EA=O221O2×100%EA = \frac{O_2}{21 - O_2} \times 100\%

From flue gas oxygen measurement.

Variables

SymbolDescriptionUnit
QQHeat release rateW
m˙\dot{m}Mass flow ratekg/s
HVHVHeating valueJ/kg
AFAFAir-fuel ratio

Definitions

Prandtl Number (Pr): A dimensionless number approximating the ratio of momentum diffusivity to thermal diffusivity. For air, it is often used in heat transfer calculations.

Specific Heat Ratio (γ): The ratio of the specific heat at constant pressure (Cp) to the specific heat at constant volume (Cv). For air, this ratio is approximately 1.4 at standard conditions.

SCFM (Standard Cubic Feet per Minute): The volumetric flow rate of a gas measured at standard conditions (typically 68°F, 14.696 psi).

ACFM (Actual Cubic Feet per Minute): The volumetric flow rate of a gas at actual operating conditions of temperature and pressure.

ICFM (Inlet Cubic Feet per Minute): The volumetric flow rate of a gas at the inlet conditions of a compressor.

Additional Key Formulas

Boyle's Law (Mariotte's Law): P1V1=P2V2P_1V_1 = P_2V_2 Relates pressure and volume of a gas at constant temperature.

Charles' Law: V1T1=V2T2\frac{V_1}{T_1} = \frac{V_2}{T_2} Relates volume and absolute temperature of a gas at constant pressure.

Prandtl Number for Air: Pr=να=μCpkPr = \frac{\nu}{\alpha} = \frac{\mu C_p}{k} Where ν\nu is kinematic viscosity, α\alpha is thermal diffusivity, μ\mu is dynamic viscosity, CpC_p is specific heat, and kk is thermal conductivity.

Specific Heat Ratio: γ=CpCv\gamma = \frac{C_p}{C_v} For dry air near standard conditions, γ1.4\gamma \approx 1.4.

Conversion between SCFM and ACFM: ACFM=SCFM×PstdPact×TactTstdACFM = SCFM \times \frac{P_{std}}{P_{act}} \times \frac{T_{act}}{T_{std}} Where P and T are absolute pressure and temperature.

References