We present FLEW, an in-house high-fidelity solver for Direct Numerical Simulation (DNS) of turbulent compressible flows over arbitrary shaped geometries. FLEW solves the Navier-Stokes equations written in a generalized curvilinear coordinate system, in which the surface coordinates are non-orthogonal, whereas the third axis is normal to the surface. Spatial discretization relies on high-order finite-difference schemes. The convective terms are discretized using a hybrid approach, combining the near-zero numerical dissipation provided by central approximations with the robustness of Weighted Essentially Non-Oscillatory (WENO) schemes, required to capture shock waves. Central schemes are stabilized using a skew-symmetric-like splitting of convective derivatives, endowing the solver with the energy- preserving property in the inviscid limit. The maximum order of accuracy is eighth for central schemes (also used for viscous terms discretization) and seventh for WENO. The code is oriented to modern High-Performance Computing (HPC) platforms thanks to Message Passing Interface (MPI) parallelization and the ability to run on Graphics Processing Unit (GPU) architectures. Reliability, accuracy, and robustness of the code are assessed in the low-subsonic, transonic, and supersonic regimes. We present the results of several benchmarks, namely the inviscid Taylor-Green vortex, turbulent curved channel flow, transonic laminar flow over a NACA 0012 airfoil and turbulent supersonic ramp flow. The results for all configurations proved to be in excellent agreement with previous studies.