TY - JOUR
T1 - Theoretical analysis on thermoacoustic dynamic responses of laminar premixed ammonia-hydrogen-air conical flames based on G-equation models
AU - Tian, Yu
AU - Luo, Qi
AU - Wang, Pengcheng
AU - Nan, Jiaqi
AU - Yang, Lijun
AU - Li, Jingxuan
N1 - Publisher Copyright:
© 2025 Elsevier Masson SAS
PY - 2025/9
Y1 - 2025/9
N2 - This paper investigates thermoacoustic dynamic responses of ammonia-hydrogen-air flames by theoretical analysis. Utilizing G-equation models, flame transfer functions (FTFs) can be obtained through a linearized analytical solution, while flame describing functions (FDFs) are derived from a fully numerical solution using the level set approach. The study examines linear FTFs under different ammonia enrichment levels (ηNH3), unstretched flame aspect ratios (β), Markstein lengths (L), and equivalence ratios (ϕ), as well as nonlinear FDFs under different normalized incoming flow velocity perturbation amplitudes. Results indicate that increasing ηNH3 enhances the flame speed, accelerating the decline in the FTF gain with frequency and reducing the propensity for thermoacoustic instability. The effect of flame curvature on increasing FTF gains and altering flame shape becomes more pronounced at small β and large L. Consequently, ammonia-hydrogen-air flames exhibit greater stability under stoichiometric conditions, as L approaches 0 across various ηNH3 and β. Finally, a comparative analysis of FDF results indicates that higher velocity perturbation amplitudes effectively reduce the flame height at smaller L. The reduction in flame front wrinkles alters the behavior of FDFs, leading to more pronounced nonlinear effects in the flame response.
AB - This paper investigates thermoacoustic dynamic responses of ammonia-hydrogen-air flames by theoretical analysis. Utilizing G-equation models, flame transfer functions (FTFs) can be obtained through a linearized analytical solution, while flame describing functions (FDFs) are derived from a fully numerical solution using the level set approach. The study examines linear FTFs under different ammonia enrichment levels (ηNH3), unstretched flame aspect ratios (β), Markstein lengths (L), and equivalence ratios (ϕ), as well as nonlinear FDFs under different normalized incoming flow velocity perturbation amplitudes. Results indicate that increasing ηNH3 enhances the flame speed, accelerating the decline in the FTF gain with frequency and reducing the propensity for thermoacoustic instability. The effect of flame curvature on increasing FTF gains and altering flame shape becomes more pronounced at small β and large L. Consequently, ammonia-hydrogen-air flames exhibit greater stability under stoichiometric conditions, as L approaches 0 across various ηNH3 and β. Finally, a comparative analysis of FDF results indicates that higher velocity perturbation amplitudes effectively reduce the flame height at smaller L. The reduction in flame front wrinkles alters the behavior of FDFs, leading to more pronounced nonlinear effects in the flame response.
KW - Ammonia-hydrogen-air flames
KW - Flame describing function
KW - Flame transfer function
KW - G-equation
KW - Thermoacoustic dynamic response
UR - https://www.scopus.com/pages/publications/105007465056
U2 - 10.1016/j.ast.2025.110398
DO - 10.1016/j.ast.2025.110398
M3 - 文章
AN - SCOPUS:105007465056
SN - 1270-9638
VL - 164
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 110398
ER -