Atmospheric Pressure Equation:
Approximate, but exponential better.
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The atmospheric pressure equation calculates the pressure at a given elevation based on initial pressure, air density, gravity, and height difference. This is a simplified linear approximation that works well for small elevation changes.
The calculator uses the pressure equation:
Where:
Explanation: The equation accounts for the weight of the air column above the measurement point. For more accurate results over larger elevation changes, the barometric formula (exponential) should be used.
Details: Accurate pressure calculation is crucial for weather forecasting, aviation, engineering applications, and understanding how pressure affects human physiology at different altitudes.
Tips: Enter all values in the specified units. Default values are provided for standard atmospheric conditions (P₀ = 101325 Pa, ρ = 1.225 kg/m³, g = 9.80665 m/s²).
Q1: Why is this equation approximate?
A: This linear approximation assumes constant air density, which isn't true for large elevation changes. The barometric formula accounts for density changes with altitude.
Q2: What are typical sea level pressure values?
A: Standard atmospheric pressure at sea level is 101325 Pa (1013.25 hPa or 1 atm).
Q3: How does temperature affect the calculation?
A: Temperature affects air density (ρ). Warmer air is less dense, resulting in less pressure change with elevation.
Q4: What's the pressure at Mount Everest's summit?
A: Approximately 33700 Pa (about 1/3 of sea level pressure) using the more accurate barometric formula.
Q5: When is this linear approximation sufficient?
A: For elevation changes less than a few hundred meters, this approximation is reasonably accurate.