Prandtl shock relation
= Prandtl shock relation
{c}
{title2=$u_1u_2=c_{\rm cr}^2$}
For a stationary normal shock in a polytropic perfect gas, the upstream and downstream normal speeds obey $u_1u_2=c_{\rm cr}^2$, where $c_{\rm cr}$ is the sonic speed on their common Bernoulli streamline.