Pressure altitude is the height of an atmospheric surface above a standard reference pressure level, typically sea level (1013.25 hPa). It is used in aviation and meteorology to determine flight levels and weather patterns.
The relationship between pressure altitude and station pressure can be described by the formula:
T0 = standard temperature at sea level (288.15 K)
g = acceleration due to gravity (9.80665 m/sΒ²)
P = station pressure (hPa)
P0 = standard atmospheric pressure at sea level (1013.25 hPa)
R = specific gas constant for dry air (287.058 J/(kgΒ·K))
Cp = specific heat capacity of air at constant pressure (1004.68 J/(kgΒ·K))
This formula accounts for the temperature variation with altitude and provides a more accurate calculation of pressure altitude compared to simpler models.
What is pressure altitude in aviation?
How do I calculate pressure altitude?
Why is pressure altitude important in aviation?
What is the standard reference pressure level for pressure altitude?
How does temperature affect pressure altitude calculations?
Can I use this calculator for non-aviation purposes?
What are some common uses of pressure altitude in meteorology?
Results are for informational purposes only and do not constitute professional advice.
