Atmospheric Pressure Equation:
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The atmospheric pressure equation describes how pressure decreases with altitude in an isothermal atmosphere. It's derived from the barometric formula and assumes constant temperature.
The calculator uses the atmospheric pressure equation:
Where:
Explanation: The equation shows exponential decrease in pressure with altitude, with rate depending on temperature and air composition.
Details: Understanding pressure variation with altitude is crucial for aviation, meteorology, engineering, and atmospheric sciences. It affects aircraft performance, weather patterns, and equipment design.
Tips: Enter height in meters, temperature in Kelvin, and base pressure in Pascals (default is sea level pressure 101325 Pa). All values must be positive.
Q1: Why does pressure decrease with altitude?
A: Pressure decreases because there's less air above pushing down as you go higher in the atmosphere.
Q2: What are typical atmospheric pressure values?
A: Standard sea level pressure is 101325 Pa (1013.25 hPa). At Mount Everest's summit (8848m), it's about 30% of sea level pressure.
Q3: How does temperature affect the result?
A: Higher temperatures make the atmosphere more expanded, so pressure decreases more slowly with altitude in warm conditions.
Q4: What are the limitations of this equation?
A: It assumes constant temperature and doesn't account for humidity or local weather variations. More complex models exist for precise calculations.
Q5: Can this be used for other planets?
A: Yes, but you'd need to adjust M (molar mass), g (gravity), and possibly R for the specific planetary atmosphere.