Air Flow over Cylindar (Under Development)¶

In this chapter we perform the numerical simulations for acoustic field generated by air flowing over a cylinder. This problem is chosen to verify the accuracy of the developed solver. The acoustic fields are calculated for different Reynolds numbers

(1) $\mathrm{Re} \defeq \frac{\rho vD}{\mu}$

The density of air is $\rho = 1.2250 \,\mathrm{kg}/\mathrm{m}^3$ . The dynamic viscosity is $\mu = 1.983\times10^{-5} \,\mathrm{kg}/\mathrm{(m\cdot s)}$ . Choose the diameter of the cylinder to be $D = 0.1 \,\mathrm{m}$ . Then, at the three given Reynolds numbers, the velocity can be calcuated from (1):

$v = \frac{\mu\mathrm{Re}}{\rho D}$

Reynolds number	89,000	46,000	22,000
Velocity (m/s)	14.407102	7.446367	3.561306

Note

In examples/bulk/air run the following commands to obtain the above numbers:

./go velocity --density 1.225 --diameter 0.1 --dvisco 1.983e-5 --reynolds 89000
./go velocity --density 1.225 --diameter 0.1 --dvisco 1.983e-5 --reynolds 46000
./go velocity --density 1.225 --diameter 0.1 --dvisco 1.983e-5 --reynolds 22000

The bulk modulus of air is $K = 1.42 \times 10^5 \, \mathrm{Pa}$ .