At point $1$ between two adjacent streamlines, the static pressure $(P_1)$ is $2040\mathrm{.}86l\frac{b}{f}{t}^2$ and airflow speed is $100f\frac{t}{sec}.$ At point $2,$ the speed of the airflow increases to $200f\frac{t}{sec}.$ Based on Bernoulli's principle, if the air density is $0\mathrm{.}002308$ slugs$/f{t}^3,$ what would be the static pressure at point $2(P_2)?$

$1806\mathrm{.}24l\frac{b}{f}{t}^2$

$2006\mathrm{.}24l\frac{b}{f}{t}^2$

$2206\mathrm{.}24l\frac{b}{f}{t}^2$

$2406\mathrm{.}24l\frac{b}{f}{t}^2$