Extension of a combined analytical/numerical initial value problem solver for turbulent mixing with combustion.

DOI10.1016/S0045-7930(03)00003-3zbMath1140.80420OpenAlexW2078895575MaRDI QIDQ1421567

Jonathan A. Seidel, Lawrence J. De Chant, Teresa R. Kline

Publication date: 26 January 2004

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(03)00003-3

zbMATH Keywords

Preliminary designAerodynamic mixingCombined analytical/numerical methodEjector nozzleElementary combustion model

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Combustion (80A25) Reaction effects in flows (76V05) Turbulent transport, mixing (76F25) Finite difference methods applied to problems in thermodynamics and heat transfer (80M20)

Cites Work

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• Higher order accurate difference solutions of fluid mechanics problems by a compact differencing technique
• A combined analytical singularity subtraction method and compact implicit differencing scheme for aerodynamic mixing
• Multiple stream superposition of a two-stream combined analytical numerical initial value problem solver for aerodynamic mixing.
• Supersonic Air Ejectors
• Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling
• Simplified turbulence modeling for forced vortical mixers using a kinematic wave analogy

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