c = √(γ R T / M), where γ = c_p/c_v is the adiabatic index, R the gas constant, T temperature, and M molar mass. Derives from treating sound as an adiabatic pressure perturbation on an ideal gas — faster than the isothermal Newton…
c = √(γ R T / M), where γ = c_p/c_v is the adiabatic index, R the gas constant, T temperature, and M molar mass. Derives from treating sound as an adiabatic pressure perturbation on an ideal gas — faster than the isothermal Newton…