Temperature-Based Calculations

Density
1.204 kg/m³
Dynamic Viscosity
1.82e-5 Pa·s
Thermal Conductivity
0.0257 W/(m·K)
Specific Heat (Cp)
1.005 kJ/(kg·K)
Speed of Sound
343.2 m/s
Prandtl Number
0.707 -

Property vs Temperature

Altitude Adjustment Mode

International Standard Atmosphere (ISA)
15.0 °C
101325 Pa
1.225 kg/m³

Altitude vs Atmospheric Properties

Humidity Effects

%
Dew Point
9.3 °C
Humidity Ratio
0.0072 kg/kg
Specific Enthalpy
38.5 kJ/kg
Specific Volume
0.84 m³/kg

Psychrometric Chart

Aviation Mode

True Airspeed (TAS)
0 m/s
Equivalent Airspeed (EAS)
0 m/s
Impact Pressure (Qc)
0 Pa
Total Temperature
0 °C

Mach Number vs Altitude