Numerical Simulation of a High-speed Jet Injected in a Uniform Supersonic Crossflow Using Adaptively Redistributed Grids
Minimizing numerical dissipation without compromising the robust shock-capturing attributes remains an outstanding challenge in the design of numerical methods for high-speed compressible flows. The conflicting requirements of low and high numerical dissipation for accurate resolution of discontinuo...
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Language: | en_US |
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2018
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Online Access: | http://etd.iisc.ernet.in/2005/3583 http://etd.iisc.ernet.in/abstracts/4451/G28174-Abs.pdf |