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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Bibliographic Details
Main Author: Seshadrinathan, Varun
Other Authors: Shukla, Ratnesh K
Language:en_US
Published: 2018
Subjects:
Online Access:http://etd.iisc.ernet.in/2005/3583
http://etd.iisc.ernet.in/abstracts/4451/G28174-Abs.pdf