Three-step approach for prediction of limit cycle pressure oscillations in combustion chambers of gas turbines

DOI10.1080/13647830.2017.1349343OpenAlexW2736981404MaRDI QIDQ5073622

Dmytro Iurashev, Vyacheslav V. Anisimov, Ezio Cosatto, Giovanni Campa

Publication date: 3 May 2022

Published in: Combustion Theory and Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/13647830.2017.1349343

zbMATH Keywords

limit cycleURANScombustion instabilitiestime-domain simulationsFSC model

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Thermodynamics and heat transfer (80Axx)

Related Items (3)

Neural network PID control for combustion instability ⋮ Sliding mode control for longitudinal oscillating combustion ⋮ Experimental investigation on critical slowing down of premixed combustion in a backward-facing step combustor

Cites Work

• Boundary conditions for direct simulations of compressible viscous flows
• Progress in the development of a Reynolds-stress turbulence closure

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