Altitude Formula:
From: | To: |
Definition: This calculator estimates altitude based on atmospheric pressure using the barometric formula.
Purpose: It's used in aviation, meteorology, and engineering to determine elevation from pressure measurements.
The calculator uses the formula:
Where:
Explanation: The formula models how atmospheric pressure decreases exponentially with altitude in an isothermal atmosphere.
Details: Accurate altitude determination is crucial for aircraft navigation, weather forecasting, and scientific research.
Tips: Enter the measured pressure, temperature (in Kelvin), and optionally adjust the constants if needed. All values must be > 0.
Q1: What's the standard sea level pressure?
A: The International Standard Atmosphere defines 101325 Pa (1013.25 hPa) as standard sea level pressure.
Q2: How does temperature affect the calculation?
A: Higher temperatures result in less dense air, making the atmosphere "taller" at a given pressure.
Q3: When would I change the gas constant?
A: The default 287 J/kg·K is for dry air. Use 461.5 J/kg·K for water vapor or adjust for specific humidity.
Q4: How accurate is this calculation?
A: It assumes an isothermal atmosphere. For greater accuracy, use the full atmospheric model with layers.
Q5: Can I use hPa instead of Pa?
A: Yes, but ensure both P₀ and P use the same units (1 hPa = 100 Pa).