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(7) where P atmospheric pressure [kPa],

z elevation above sea level [m], Source: FAO meterological handbook.

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The formula to convert elevation to atmospheric pressure is given by the barometric formula: P = P0 * exp(-Mgh / (R*T)), where P is the atmospheric pressure at elevation h, P0 is the atmospheric pressure at sea level, M is the molar mass of air, g is the acceleration due to gravity, R is the ideal gas constant, and T is the temperature in Kelvin.

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Q: What is the formula to convert elevation to atmospheric pressure?
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What is the atmospheric pressure if the temperature is at 0c the velocity of sound is 331.0ms density of air is 1.295kg and what formula is used?

The atmospheric pressure can be calculated using the ideal gas law formula: P = ρRT, where P is the pressure, ρ is the density, R is the gas constant, and T is the temperature. The value of the gas constant depends on the units used for pressure, density, and temperature. Given the values provided, the gas constant should be 287 J/(kg·K) for pressure in Pascals, density in kg/m^3, and temperature in Kelvin. Plug in the values and calculate the pressure.