Self-excited noise generation from laminar methane/air premixed flames in thin annular jets

https://doi.org/10.1016/j.expthermflusci.2020.110321Get rights and content

Highlights

  • Various flame shapes were observed including steady and unsteady crown shaped flames.

  • Self-excited noise was generated from the unsteady crown shaped flames.

  • A frequency doubling phenomena has also been observed.

  • The calculated sound pressure from the CH* was in agreement with the measured one.

Abstract

Self-excited noise generation from laminar flames in thin annular jets of premixed methane/air has been investigated experimentally. Various flame shapes were observed in this flow configuration, including conical shaped flames, ring shaped flames, steady crown shaped flames, and oscillating crown shaped flames. Self-excited noise with a total sound pressure level of about 70 dB was generated from the oscillating crown shaped flames for equivalence ratios>0.95. Sound pressure and CH* chemiluminescence were measured by using a microphone and a photomultiplier tube. The frequency of generated noise was measured as a function of equivalence ratio and premixture velocity. A frequency doubling phenomenon has also been observed. The measured CH* chemiluminescence data were analysed and which the corresponding sound pressure has been calculated. By comparing the measured and calculated sound pressures, the noise source can be attributed to the flame front fluctuation near the edge of the oscillating crown shaped flames. The flame stability regime was influenced strongly by the mass flow rate of air through the inner tube.

Introduction

Recent demands for high combustion loads and stringent emission requirements frequently induce combustion instabilities. Since these are undesirable sources of noise and can sometimes cause disastrous destruction of combustion equipment, active control of combustion instabilities becomes one of the key interests in combustion research. In order to develop effective control technologies, it is required to understand the mechanisms and the influencing factors governing combustion instabilities.

Previous studies on unsteady combustion instabilities have frequently focused on propulsion systems such as rocket motors [1], [2], [3], jet engine afterburners [4], [5], and ramjets [6], [7], [8], [9]. These phenomena are coupled by complex, feedback-type interactions between flow, acoustics, and combustion processes. Recently, attention has been focused on the source of combustion noise by investigating relatively simple and well-defined flow geometries [10], [11], [12]. The investigation of laminar jet flames impinging on a cool plate has shown that the source of sound generation is from periodic sudden extinction of large portion of the flame interacting with the cool plate [13]. The response of burner-stabilized flat flames to acoustic velocity perturbations has also been investigated numerically and analytically [14]. These studies utilized the forcing of the flow fields by acoustic speakers. Studies of self-excited combustion noise generation in simple laminar flow geometries are rather limited.

Although multi-coaxial burners are widely used in the field of material synthesis such as fine particle production, not many experimental studies on the characteristics of the related flames have been conducted [15], [16]. In this study, the characteristics of various flames that can be formed in a double coaxial burner were investigated, and the structure and stability of the flame were investigated.

This type of flow geometry has been investigated previously in terms of flame stabilization [17]. Self-excited combustion noise has been generated which depends on the equivalence ratio and jet velocity [18], [19]. The present study focuses on the self-excited noise generation in the burner, especially the regimes and overall characteristics of noise generation.

Section snippets

Experimental apparatus

The apparatus consisted of an annular jet burner and flow controllers, a visualization setup, and a sound pressure measurement system. The annular jet burner, shown schematically in Fig. 1, was composed of double concentric tubes, which were made of brass. The inner tube is 400 mm long with i.d. 10.1 mm and o.d. 10.9 mm. The outer tube was 300 mm long with i.d. 12.8 mm and o.d. 13.8 mm. The resonance frequency of the inner tube was 425 Hz. The annular slit width was 0.95 mm and the exit area of

Observed flames

Various flame types have been observed depending on the equivalence ratio ϕ and mixture velocity Up. Direct photographs of typical flame types are shown in Fig. 2 for the air velocity in the inner tube Ua = 0. The Reynolds number is defined as Up⋅De, where ν is the kinematic viscosity, De is the hydraulic diameter based on the flow rate, that is, De = Dout − Din, Dout is the i.d of the outer tube, and Din is the o.d. of the inner tube. The Strouhal number is defined as f⋅De/Up, where f is the

Concluding remarks

Premixed methane/air flames in the laminar thin annular jet burner have been studied experimentally to investigate the characteristics of self-excited noise generation. The flame in the annular jets has various flame shapes, including ring shaped, near conical shaped, crown shaped, and oscillating crown shaped depending on equivalence ratio, mixture velocity and air velocity. The regimes of the existence of these flames were identified. Self-excited noise with an SPL of about 70 dB was

CRediT authorship contribution statement

Seong-Ho Jin: Methodology, Writing - original draft, Investigation, Writing - review & editing. Jae-Hoon Joung: Investigation. Suk-Ho Chung: Supervision.

Declaration of Competing Interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

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