A time-accurate scheme for the calculations of unsteady reactive flows at low Mach number

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1097-0363(19990130)29:2<207::AID-FLD785>3.0.CO;2-5" /><207::AID-FLD785>3.0.CO;2-5 10.1002/(SICI)1097-0363(19990130)29:2<207::AID-FLD785>3.0.CO;2-5zbMath0939.76059OpenAlexW1980022012MaRDI QIDQ4254676

No author found.

Publication date: 5 July 2000

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(19990130)29:2<207::aid-fld785>3.0.co;2-5

zbMATH Keywords

sensitivity analysisconvergence ratelow Mach numberartificial compressibility methodpremixed turbulent combustioneddy break-up-like approachplanar turbulent flameunsteady turbulent reacting flows

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Shear flows and turbulence (76F10) Chemically reacting flows (80A32) Reaction effects in flows (76V05)

Cites Work

• Theory of Laminar Flames

This page was built for publication: A time-accurate scheme for the calculations of unsteady reactive flows at low Mach number