MODELING OF SUPERSONIC COMBUSTION USING POINT IMPLICIT FINITE VOLUME METHOD

DOI10.1142/S0219876207001060zbMath1198.76074OpenAlexW2060166183MaRDI QIDQ3056056

Sadanand Sadashiv Gokhale, Mukundan Nair Deepu

Publication date: 10 November 2010

Published in: International Journal of Computational Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0219876207001060

zbMATH Keywords

stiffnesssupersonic combustionpoint implicit finite volume method

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Combustion (80A25) Reaction effects in flows (76V05) Supersonic flows (76J20)

Cites Work

• Numerical study on supersonic combustion with cavity-based fuel injection
• Finite-volume method for the calculation of compressible chemically reacting flows
• Development of turbulence models for shear flows by a double expansion technique

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