A fully implicit time accurate method for hypersonic combustion: Application to shock-induced combustion instability
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Publication:2564128
DOI10.1007/BF02425222zbMath0889.76055OpenAlexW2020832507MaRDI QIDQ2564128
Shaye Yungster, Krishnan Radhakrishnan
Publication date: 7 January 1997
Published in: Shock Waves (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf02425222
Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Combustion (80A25) Reaction effects in flows (76V05) Hypersonic flows (76K05)
Related Items (6)
An improved uncoupled finite volume solver for simulating unsteady shock-induced combustion ⋮ A hybrid LES (large eddy simulation)/assumed sub-grid PDF (probability density function) model for supersonic turbulent combustion ⋮ A spectral radius scaling semi-implicit iterative time stepping method for reactive flow simulations with detailed chemistry ⋮ Computational study of NOx formation in hydrogen-fuelled pulse detonation engines ⋮ Computational study of NOx formation in hydrogen-fuelled pulse detonation engines ⋮ A solver for simulating shock-induced combustion on curvilinear adaptive meshes
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