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Interfaces and discontinuities occur in a variety of computational
problems ranging from engineering to computer graphics and a
great deal of theoretical and computational effort is usually
required to produce numerical algorithms to treat these types
of problems. Moreover, these algorithms tend to be complicated
and problem specific as one has to enforce the appropriate boundary
conditions at the interface or discontinuity. A new numerical
technique, the Ghost Fluid Method, has recently been developed
to handle interfaces in a robust and efficient fashion leading
to a general class of "boundary condition capturing"
techniques that can easily be applied to a large number of problems.
These techniques are based on identification of "continuous"
and "discontinuous" variables at an interface and
treating these variables so that one can difference across the
interface in a seamless and simple fashion. It is important
to note that a special definition of "continuous"
is used, e.g. we will define 3 continuous variables across a
one-dimensional shock wave.
Back to High-Speed Combustion in Gaseous and Condensed-Phase Energetic Materials
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