Atmospheric Pressure Elevation Formula:
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The Atmospheric Pressure Elevation Formula calculates the atmospheric pressure at a given elevation based on sea level pressure, temperature, and other physical constants. It's derived from the barometric formula and accounts for the decrease in pressure with altitude.
The calculator uses the atmospheric pressure elevation formula:
Where:
Explanation: The formula models how atmospheric pressure decreases with altitude in the troposphere, assuming a constant temperature lapse rate.
Details: Accurate pressure calculation at different elevations is crucial for aviation, meteorology, engineering, and scientific research. It affects aircraft performance, weather prediction, and equipment calibration.
Tips: Enter sea level pressure in Pascals, elevation in meters, temperature in Kelvin, gravitational acceleration in m/s², and gas constant in J/kg·K. Default values are provided for standard atmospheric conditions.
Q1: What are typical values for sea level pressure and temperature?
A: Standard sea level pressure is 101325 Pa (1 atm) and standard temperature is 288.15 K (15°C).
Q2: How accurate is this formula?
A: It provides good estimates for elevations within the troposphere (up to about 11 km). For higher altitudes, different models are needed.
Q3: Why does pressure decrease with altitude?
A: Pressure decreases because there's less atmospheric mass above as you go higher, and gravity's pull on the air molecules weakens.
Q4: What's the temperature lapse rate?
A: The rate at which temperature decreases with altitude (0.0065 K/m in the troposphere).
Q5: Can I use this for weather station pressure correction?
A: Yes, this formula can help adjust pressure measurements to sea level for comparison with standard values.