Article
Thermodynamics
Liang Yu, B. Aravind, Deanna A. Lacoste
Summary: This paper demonstrates that nanosecond repetitively pulsed discharges can reduce the response of lean methane-air swirl flames to acoustic excitations at pressures up to 3 bar. The flame transfer functions with and without plasma discharges were studied in the frequency range of 48-380 Hz at pressures of 1.2, 2.0, and 3.0 bar. The results show that the plasma discharges can decrease the gain of the flame transfer functions by up to 50%, regardless of the pressure. The mechanisms responsible for this effect are discussed.
COMBUSTION AND FLAME
(2023)
Article
Thermodynamics
Ajit Kumar Dubey, Takuya Tezuka, Youhi Morii, Hisashi Nakamura, Kaoru Maruta
Summary: Acoustic and parametric instability in downward propagating premixed flames of low Lewis number mixtures were studied experimentally and analytically. The results show that parametric instability of the flame front due to the effect of acoustics occurs when the laminar burning velocity of the mixture exceeds 27 cm/s. Furthermore, there is a quantitative agreement between the experimental and theoretical results, demonstrating the applicability of theoretical analysis for low Lewis number mixtures.
COMBUSTION AND FLAME
(2023)
Article
Thermodynamics
Maria Castela, Alam Garciduenas Correa, Jason S. Damazo, Deanna A. Lacoste
Summary: Experimental study on thermoacoustic coupling of methane flames in small diameter tubes revealed that thermoacoustic instability impacts flame propagation and can lead to flame quenching. Depending on the tube length (acoustics), flames either fully propagate or extinguish prematurely.
COMBUSTION AND FLAME
(2021)
Article
Mechanics
Meng Han, Xiao Han, Jianchen Wang, Xianzhi Gao, Pei He, Xiaoxing Feng, Yuchen Zhou
Summary: This study focuses on the effect of air split ratio (ASR) on thermoacoustic instability in lean premixed combustors. It is found that thermoacoustic instability is suppressed with ASR higher than 20%. The pilot flame becomes longer and the main flame becomes shorter with increasing ASR, and the separation between the two flames decreases. The present study demonstrates that a higher air split ratio improves thermoacoustic stability in designing LPM combustors.
Article
Engineering, Aerospace
Zhuming Rao, Ruichao LI, Peizhe Zhao, Bing Wang, Dan Zhao, Qiaofeng Xie
Summary: This study experimentally investigated the flame responses to acoustic disturbances with different frequencies and amplitudes in a combustor operating at different bulk velocities. The results showed that low-frequency disturbances caused drastic oscillations in the heat release rate and high-order harmonics. Increasing the bulk velocity extended the frequency range for flame response and reduced the delay time. A non-dimensional parameter was introduced to capture the similarity among flame responses at different bulk velocities.
CHINESE JOURNAL OF AERONAUTICS
(2023)
Article
Engineering, Aerospace
Yongchao Sun, Mingbo Sun, Dan Zhao, Yong Chen, Guangwei Ma, Minggang Wan, Yuze Sun, Jiajian Zhu
Summary: In this study, systematic experiments and numerical simulations were conducted to investigate the interaction between a premixed methane/air flame and acoustic disturbances in a longitudinal combustor, with a focus on blow-off characteristics. The results showed that the flame height increment was significantly affected by the evolution of vortices in the unburnt gas, leading to flame blow-off at an excitation frequency of 260 Hz. Experimental and numerical findings shed light on the fundamental physics of a premixed flame response to acoustic disturbances.
AEROSPACE SCIENCE AND TECHNOLOGY
(2021)
Article
Chemistry, Physical
Qiang An, Sina Kheirkhah, Jeffrey Bergthorson, Sean Yun, Jeongjae Hwang, Won June Lee, Min Kuk Kim, Ju Hyeong Cho, Han Seok Kim, Patrizio Vena
Summary: Flame shapes and transitions of premixed hydrogen enriched methane flames in a 3D-printed low-swirl burner were studied. Three different flame shapes were observed, each stabilized by different mechanisms such as flame-flow velocity balance, inner shear layer, large-scale eddies in the outer shear layer, and burner hardware anchorage. The transitions between flame shapes were mainly influenced by hydrogen fraction and bulk velocity, with the W-to-crown transition attributed to the upstream propagation and attachment of the flame outer edges.
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
(2021)
Article
Energy & Fuels
Yunpeng Liu, Yingwen Yan, Shoutang Shang, Hongyu Ma
Summary: Combustion instability, which refers to the thermoacoustic coupling problem in combustion systems, can result in damaging pressure oscillations. Understanding the mechanism and triggering problem of combustion instability is crucial. This study adopted experimental methods to measure the flame transfer function and flame describing function that govern pressure pulsation, and investigated the impact of heat release rate fluctuation on acoustic disturbance. The results revealed complex curvature of flame pulsation amplitude at frequencies lower than 200 Hz, and the growth rate of pulsation amplitude decreased monotonically with increasing frequencies above 200 Hz. The concept of a trigger threshold for low-frequency oscillation was verified through self-excited combustion instability tests.
Article
Thermodynamics
Jianyi Zheng, Sirui Wang, Zifeng Yang, Lei Li, Guoqing Wang, Yi Gao, Xunchen Liu, Fei Qi
Summary: A dual-plane stereoscopic particle image velocimetry (PIV) technique is used to investigate the dynamics of periodically-excited vortices in a swirling flame. Results show that the external vortex rings (OVRs) and internal vortex rings (IVRs) exhibit opposite rotational characteristics under different excitation frequencies. The amplitude and phase of oscillation velocities in three directions are successfully decomposed, and it is found that the vortex rings contribute to the axial velocity oscillations.
EXPERIMENTAL THERMAL AND FLUID SCIENCE
(2022)
Article
Mathematics, Applied
Ankit Sahay, Abhishek Kushwaha, Samadhan A. A. Pawar, P. R. Midhun, Jayesh M. M. Dhadphale, R. I. Sujith
Summary: In this study, amplitude death (AD) of limit cycle oscillations in a bluff body stabilized turbulent combustor is achieved through delayed acoustic self-feedback. We found that the complete suppression of these oscillations occurs when the length of the coupling tube is approximately 3/8 times the wavelength of the fundamental acoustic mode. Furthermore, by applying delayed acoustic self-feedback with optimum parameters, the positive feedback loop between hydrodynamic, acoustic, and heat release rate fluctuations in the combustor can be disrupted, mitigating thermoacoustic instability.
Article
Thermodynamics
Ajit Kumar Dubey, Yoichiro Koyama, Nozomu Hashimoto, Osamu Fujita
Summary: This study investigates thermo-acoustic instability in a mesoscale tube of diameter 8 mm, revealing different flame responses for mixtures with different Lewis numbers. Flame extinction due to heat loss and the formation of parametric cellular structures are observed, with the diameter of the tube playing a key role in determining the type of flame response. The suppression of acoustic parametric instability for higher burning velocity mixtures and the occurrence of beating instability for CO2 diluted mixtures of Le > 1 are also discussed.
COMBUSTION AND FLAME
(2021)
Article
Engineering, Environmental
Tao Cai, Aikun Tang, Chong Li
Summary: This study reveals the flame dynamics and stability of ammonia/hydrogen co-firing combustion using experimental and numerical techniques. Experimental results confirm five types of micro-flame structures and delineate a flame stability diagram. The study shows that increasing the blending ratio extends the blowoff limit and enhances flame stability.
CHEMICAL ENGINEERING JOURNAL
(2023)
Article
Thermodynamics
Douglas B. Proud, Michael J. Evans, Qing N. Chan, Paul R. Medwell
Summary: This study investigates the structure and stabilisation mechanisms of ethanol and n-heptane spray flames using laser diagnostic techniques. The results show a noticeable shift in flame stabilisation behavior with variations in coflow oxygen concentration, while coflow temperature does not seem to have a significant impact. These flames exhibit interesting deviations from typical behaviors observed in gaseous and prevaporised flames in similar configurations, especially for coflow conditions associated with the transition to the mild combustion regime.
COMBUSTION AND FLAME
(2022)
Article
Thermodynamics
Vadim N. Kurdyumov, Carmen Jimenez
Summary: This study investigates the structure and dynamics of premixed flames in narrow channels with a highly conductive wall segment. The findings reveal the existence of multiple steady-state regimes, with several steady solutions being simultaneously stable. The stability analysis is confirmed by time-dependent simulations, which also demonstrate the possibility of nonlinear periodic and chaotic dynamics under certain conditions.
COMBUSTION AND FLAME
(2022)
Article
Thermodynamics
Nikhil Balasubramanian, Dongang Cao, Inbar Greenberg, Dan Michaels
Summary: This paper investigates the effects of injecting diluent gas into the outer recirculation zone of a swirl stabilized premixed methane/air flame on flame shape and combustion dynamics. The study identifies two modes of instability and demonstrates the influence of different diluent gas compositions on flame stability.
COMBUSTION AND FLAME
(2022)