Zobrazeno 1 - 10
of 1 601
pro vyhledávání: '"combustion instability"'
Autor:
Seonyeong Kim, Daesik Kim
Publikováno v:
Case Studies in Thermal Engineering, Vol 59, Iss , Pp 104595- (2024)
In this study, the effects of various system parameters on combustion instability were numerically identified through a network-based thermoacoustic model using the concept of a transfer function. The acoustic transfer function was derived from the w
Externí odkaz:
https://doaj.org/article/27673e1911574816b3d6775abeaedc1b
Publikováno v:
Applied Sciences, Vol 14, Iss 20, p 9419 (2024)
Blowoff limits are essential in establishing the combustor operating envelope. Hence, there is a great demand for practical aero-engines to extend the blowoff limits further. In this work, the behavior of non-premixed swirling flames under fuel flow
Externí odkaz:
https://doaj.org/article/ef0585ec5fda4abe8a7dfdf3460e6438
Publikováno v:
Aerospace, Vol 11, Iss 9, p 759 (2024)
Acoustic instabilities in solid rocket motors (SRMs) can lead to severe performance deterioration and structural damage. Nozzle damping accounts for the main acoustic dissipation source, and it is highly dependent on geometric parameters and operatin
Externí odkaz:
https://doaj.org/article/fabccfc676664ab3bd713950a0858e5c
Publikováno v:
Energies, Vol 17, Iss 16, p 4164 (2024)
This study focuses on the center-staged swirl model combustion chamber, conducting experiments and numerical simulations to investigate the unstable combustion characteristics of diffusion flames under different Reynolds numbers and air–fuel ratios
Externí odkaz:
https://doaj.org/article/65f6837f66fd42a6ba822a0bf209c803
Publikováno v:
Aerospace, Vol 11, Iss 6, p 455 (2024)
This paper investigates the role of chaotic analysis and deep learning models in combustion instability predictions. To detect the precursors of impending thermoacoustic instability (TAI) in a swirled combustor with various fuel injection strategies,
Externí odkaz:
https://doaj.org/article/2ecaba55144b4cc08f9bb0e01a9ea78c
Publikováno v:
Energies, Vol 17, Iss 7, p 1639 (2024)
Pressure and flame surface oscillations are common in supersonic combustion instability. Understanding the characteristics, generation, maintenance, and interaction mechanisms of these oscillations is crucial. An experimental setup with an alcohol he
Externí odkaz:
https://doaj.org/article/cdbd93af8d8143dc8b0d17a74afc7c6e
Akademický článek
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Publikováno v:
Comptes Rendus. Mécanique, Vol 351, Iss S2, Pp 77-95 (2023)
This work is one of the analytical approaches to evaluate the evaporation frequency response of injected droplets, using the Heidmann analogy of a single droplet that is continuously fed with the same liquid fuel. Based on a linear analysis using the
Externí odkaz:
https://doaj.org/article/4e1da0f460f24c1999ae13305ffc6e0c
Publikováno v:
发电技术, Vol 43, Iss 6, Pp 927-934 (2022)
Combustion instability is easy to occur under lean combustion of gas turbine. Analyzing and predicting the characteristics of unstable combustion is of great significance to ensure the normal operation of combustion chamber. The flame describing func
Externí odkaz:
https://doaj.org/article/bb93d0bb03c04fb0bdc2cd0784aeb489