  In $\R^2$, a symmetric blunt body $W_b$ is fixed by smoothing out the tip of
a symmetric wedge $W_0$ with the half-wedge angle $\theta_w\in (0,
\frac{\pi}{2})$. We first show that if a horizontal supersonic flow of uniform
state moves toward $W_0$ with a Mach number $M_{\infty}>1$ sufficiently large,
%depending on $\theta_w$, then there exist two shock solutions, {\emph{a weak
shock solution and a strong shock solution}}, with the shocks being straight
and attached to the tip of the wedge $W_0$. Such shock solutions are given by a
shock polar analysis, and they satisfy entropy conditions. The main goal of
this work is to construct a detached shock solution of the steady Euler system
for inviscid compressible irrotational flow in $\R^2\setminus W_b$. In
particular, we seek a shock solution with the far-field state being the strong
shock solution obtained from the shock polar analysis. Furthermore, we prove
that the detached shock forms a convex curve around the blunt body $W_b$ if the
Mach number of the incoming supersonic flow is sufficiently large, and if the
boundary of $W_b$ is convex.
