T-Rex grid is applied on the surface of NLF(2)-0414F natural laminar flow airfoil. This approach provides extremely high resolution near the boundary without wasting computational power at the farfield. 

The boundary layer is resolved well with the T-Rex mesh applied, as shown in the figures above. (The length of arrows represents the magnitude of relative velocity.)

The New Glenn rocket reentry case is analyzed at Mach 5 & 15,000 Meter pressure altitude. The mesh is adapted per the criteria for higher wake resolution.

The Business jet (ATMOS 750) designed in Preliminary Design Class (AE420) is meshed and analyzed at its maximum cruising speed. The contour of Pressure, Mach number, and wall Y+ are shown above; the coefficients are presented in the report attached below.