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Theoretical analysis on thermoacoustic dynamic responses of laminar premixed ammonia-hydrogen-air conical flames based on G-equation models

  • Beihang University
  • Shanghai Institute of Space Propulsion
  • Shanghai Engineering Research Center of Space Engine
  • National Key Laboratory of Aerospace Liquid Propulsion

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Article number110398
JournalAerospace Science and Technology
Volume164
DOIs
StatePublished - Sep 2025

Keywords

  • Ammonia-hydrogen-air flames
  • Flame describing function
  • Flame transfer function
  • G-equation
  • Thermoacoustic dynamic response

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