Accounting for mean flow effects in a zero-Mach number thermo-acoustic solver : application to entropy induced combustion instabilities
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- Type
- preprint
- Published
- 2013-11-15
- Cited by
- 0
- References
- 139
- Access
- Open access
- OpenAlex
- https://openalex.org/W194919590
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:91838180
Keywords
Mach number, Combustor, Mean flow, Mechanics, Helmholtz free energy
References
- Numerical Study of Mach Number Effects on Combustion Instability
- Combustion Instabilities In Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, and Modeling
- Actively-tuned passive control of combustion instabilities
- Unsteady Motions in Combustion Chambers for Propulsion Systems
- Theoretical and numerical combustion
- Indirect combustion noise
- Thermoacoustic instabilities : Should the Rayleigh criterion be extended to include entropy changes?
- Thermoacoustic limit cycles in a premixed laboratory combustor with open and choked exits
- Quasisteady aero-acoustic response of orifices.
- Use of Finite Element Methods in Frequency Domain Aeroacoustics
- Comparison and extension of methods for acoustic identification of burners
- A generalized acoustic analogy
- Effect of flow on the acoustic resonances of an open‐ended duct
- Experimental Study on the Effect of Swirler Geometry and Swirl Number on Flame Describing Functions
- Acoustic transmission properties of a jet pipe with subsonic jet flow: I. The cold jet reflection coefficient
- Influence of the Combustor Aerodynamics on Combustion Instabilities From Equivalence Ratio Fluctuations
- Impact of Linear Coupling on the Design of Active Controllers for the Thermoacoustic Instability
- Damping and reflection coefficient measurements for an open pipe at low Mach and low Helmholtz numbers
- Modeling the damping properties of perforated screens traversed by a bias flow and backed by a cavity at low Strouhal number
- Advances in combustion and propulsion applications
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