One Solver for All Mach Numbers and Flow Conditions

  • Flow regimes between Mach numbers from 0 to much larger than 1 can simultaneously exist in the computational domain.
  • FlowVision’s general Navier-Stokes solver is capable of resolving subsonic, transonic, supersonic and hypersonic flows (Mach numbers from 0 to very large).
  • This avoids necessity of using different solvers in a solution.
  • Users are not expected to manually address regions of different flow regimes and shock generation points.


Try FlowVision…
Contact us for a technical discussion.