Physical Properties for Methane – CH4 Temperature (-50… 500°C): CelsiusFahrenheitKelvin Pressure (1… 20 bar): PascalBarAtmosphere Results: Temperature: Pressure: Molar Mass: Gas Constant: Heat Capacity Ratio: Density: Dynamic Viscosity: Kinematic Viscosity: Thermal Conductivity: Specific Heat Capacity, Cp: Specific Heat Capacity, Cv: Thermal Diffusivity: Prandtl Number: Speed of Sound:
Physical Properties for Carbon Monoxide – CO Temperature (-50… 500°C): CelsiusFahrenheitKelvin Pressure (1… 20 bar): PascalBarAtmosphere Results: Temperature: Pressure: Molar Mass: Gas Constant: Heat Capacity Ratio: Density: Dynamic Viscosity: Kinematic Viscosity: Thermal Conductivity: Specific Heat Capacity, Cp: Specific Heat Capacity, Cv: Thermal Diffusivity: Prandtl Number: Speed of Sound:
Physical Properties for Carbon Dioxide – CO2 Temperature (-50… 500°C): CelsiusFahrenheitKelvin Pressure (1… 20 bar): PascalBarAtmosphere Results: Temperature: Pressure: Molar Mass: Gas Constant: Heat Capacity Ratio: Density: Dynamic Viscosity: Kinematic Viscosity: Thermal Conductivity: Specific Heat Capacity, Cp: Specific Heat Capacity, Cv: Thermal Diffusivity: Prandtl Number: Speed of Sound:
Physical Properties for Argon Temperature (-50… 500°C): CelsiusFahrenheitKelvin Pressure (1… 20 bar): PascalBarAtmosphere Results: Temperature: Pressure: Molar Mass: Gas Constant: Heat Capacity Ratio: Density: Dynamic Viscosity: Kinematic Viscosity: Thermal Conductivity: Specific Heat Capacity, Cp: Specific Heat Capacity, Cv: Thermal Diffusivity: Prandtl Number: Speed of Sound:
XFOIL: Detailed Overview of the Airfoil Design and Analysis Tool Technology and Features: XFOIL is an open-source computational tool developed by Mark Drela at MIT that is designed for the design and analysis of subsonic isolated airfoils. It is primarily a software package that combines viscous and inviscid analysis methods with a coupling algorithm to
