Estimate the speed of sound in air at standard temperature and pressure. The mass of 1 mole of air is kg.
Step 1: Calculate density of air at STP
We know that 1 mole of any gas occupies 22.4 litres at STP. Therefore, density of air at STP is:
ρ = mass of one mole of air / volume of one mole of air at STP
ρ = (⁻³ kg) / (⁻³ m³) = 1.29 kg m⁻³
Step 2: Apply Newton's formula
According to Newton's formula, speed of sound in a gas is:
v =
At STP, P = ⁵ N m⁻²
v = \sqrt{$$1.01 \times 10$$⁵ / 1.29} = 280 m s⁻¹
Step 3: Apply Laplace correction
Newton assumed isothermal conditions, but pressure variations during sound propagation are adiabatic. Using Laplace correction:
v =
For air, γ = 7/5 = 1.4
v = = × 280 = 331.3 m s⁻¹
This agrees with the experimental value.
Explanation
The textbook demonstrates that Newton's isothermal assumption gives 280 m/s, which is 15% lower than the experimental value. Laplace corrected this by recognizing that sound propagation involves adiabatic (not isothermal) pressure variations, leading to the formula v = . Using γ = 7/5 for air yields 331.3 m/s, matching experimental observations.
Solution Steps
Step 1: Calculate density ρ = (⁻³ kg)/(⁻³ m³) = 1.29 kg m⁻³
Step 2: Apply Newton's formula v = = \sqrt{$$1.01 \times 10$$⁵/1.29} = 280 m s⁻¹
Step 3: Apply Laplace correction v = = \sqrt{$$1.4 \times 1.01$$ × 10⁵/1.29} = 331.3 m s⁻¹