Transformation of the Hypersonic Compressible Navier-Stokes Equations.
NAVAL ACADEMY ANNAPOLIS MD DIV OF ENGINEERING AND WEAPONS
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A transformation for the hypersonic compressible Navier-Stokes equations which to a large extent eliminates the necessity of specifying far field andor boundary condition parameters is presented. Both no-slip no-temperature jump and first-order velocity slip and temperature jump surface boundary conditions are considered. The transformation should be of interest to investigators seeking numerical or analytical solutions for the Navier-Stokes equations. Author
- Numerical Mathematics
- Fluid Mechanics