Unified methods for computing incompressible and compressible flow

Computation of incompressible and compressible flow generally depends on the Mach number M, where for a range of zero to supersonic compressible equations are applied but with a possible error on a range of M<0.2. For this range we have to apply incompressible Navier Stokes and Euler equations but the work would be much easier if we find a Unified Method for solving both the flows. Unified method can also lead us towards much more accuracy and efficiency.

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