Barometric Formula:
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The barometric formula describes how atmospheric pressure decreases with altitude in an isothermal atmosphere. It's derived from the ideal gas law and the hydrostatic equation, assuming constant temperature and gravitational acceleration.
The calculator uses the barometric formula:
Where:
Explanation: The formula shows exponential decrease of pressure with altitude, with the rate of decrease depending on atmospheric composition and temperature.
Details: Accurate pressure calculation is crucial for aviation, meteorology, engineering, and understanding atmospheric phenomena. It affects aircraft performance, weather patterns, and equipment design.
Tips: Enter all parameters in consistent units. Default values represent standard Earth conditions (P₀=101325 Pa, g=9.80665 m/s², M=0.0289644 kg/mol, R=8.31446 J/mol·K, T=288.15 K).
Q1: Why does pressure decrease with altitude?
A: Pressure decreases because there's less atmospheric mass above higher altitudes exerting downward force due to gravity.
Q2: What are typical pressure values at different altitudes?
A: At sea level: ~1013 hPa, at 5500m: ~500 hPa, at 16000m: ~100 hPa, at 30000m: ~10 hPa.
Q3: How does temperature affect the result?
A: Higher temperatures result in slower pressure decrease with altitude (atmosphere expands), while colder temperatures cause faster pressure decrease.
Q4: Are there limitations to this formula?
A: It assumes constant temperature and gravity, and doesn't account for atmospheric variations or weather systems. More complex models exist for precise applications.
Q5: Can this be used for other planets?
A: Yes, with appropriate values for P₀, g, M, and T for the specific planetary atmosphere.