What Is the Density of Air at a Given Temperature and Pressure?

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The density of air can be calculated using the bulk modulus and the speed of sound, with the formula B = v^2 * p. At normal atmospheric pressure and a temperature where the speed of sound in air is 339.5 m/s, the density can be derived. The density of air decreases with altitude, with values around 1.225 kg/m3 at sea level and approximately 0.841 kg/m3 at 12,000 ft. Additionally, the density of air is noted to be 0.0012 kg/m3 at 0 °C and 101.325 kPa. Understanding these relationships is crucial for accurate calculations in various applications.
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what is the density of air?

Homework Statement



For a gas at pressure P, the Bulk modulus B (under adiabatic conditions of change) is g · P. At a certain temperature, at normal atmospheric pressure, the velocity of sound in air is found to be 339.5 m/s. If g for air is 1.40, what is the density of air (in kg/m3) at that temperature ?

2. The attempt at a solution

Given wavelength, and v, then I found f:

f = v / wavelength = 242.5 Hz.

I know that:

B = v^2 * p

and B = wavelength * P

=> v^2 * p = wavelength * P

but how to find P?

I need it in couple of hours. Please advise!

Thanks a lot!
 
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Air density, like air pressure, decreases with increasing altitude. The density of the air at sea level is about 1.225 kg/m3. At 12,000 ft the density of the air is about 0.841 kg/m3.

The density of air is 0.0012 kg/m3 at 0 °C and 101.325 kPa.
 
Last edited:
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