Sound emission from a turbulent flame

1988 ◽  
Vol 21 (1) ◽  
pp. 1543-1550 ◽  
Author(s):  
Masashi Katsuki ◽  
Yukio Mizutani ◽  
Mototaka Chikami ◽  
Taizo Kittaka
2020 ◽  
Vol 12 ◽  
pp. 175682772095690
Author(s):  
S Herff ◽  
K Pausch ◽  
H Nawroth ◽  
S Schlimpert ◽  
CO Paschereit ◽  
...  

The acoustic field of a turbulent lean cpremixed open flame is numerically investigated by a hybrid method solving the Navier-Stokes equations in a large-eddy simulation formulation and the acoustic perturbation equations. The interaction of acoustic modes of a burner plenum and the turbulent flame is analyzed with respect to the sound emission of the flame. It is investigated if a simplified computation yields a good broadband agreement of the sound pressure spectrum with experimental measurements. The results of two numerical setups, i.e., the first configuration consists of the burner plus the plenum geometry while in the second configuration the plenum is neglected, which is often done in technical applications due to computational efficiency reasons, are compared with experimental findings. It can be concluded that the plenum has a pronounced impact on the dynamics and combustion noise of the open flame. To be more precise, the comparative juxtaposition of the numerical and experimental results shows a good agreement only for the full burner-plenum computation since the interaction of the acoustic quarter-wave modes of the burner plenum with the jet flow has to be captured. The interaction of these quarter-wave modes with the flow is analyzed and the acoustic response to heat release fluctuations of the flame of the full burner-plenum computation is compared to that of the simplified burner computation, in which the plenum acoustics is neglected. Due to the excitation by the plenum acoustics, the jet flow of the full burner plenum contains higher turbulent kinetic energy and the flame is excited at several additional frequencies which result in distinct peaks in the acoustic spectrum and a higher overall sound pressure level.


AIAA Journal ◽  
2002 ◽  
Vol 40 ◽  
pp. 1355-1362
Author(s):  
J. C. Hermanson ◽  
R. Sangras ◽  
J. E. Usowicz ◽  
H. Johari
Keyword(s):  

Author(s):  
Stephan Schlimpert ◽  
Seong Ryong Koh ◽  
Antje Feldhusen ◽  
Benedikt Roidl ◽  
Matthias H. Meinke ◽  
...  

2021 ◽  
Vol 230 ◽  
pp. 111432
Author(s):  
Bin Jiang ◽  
Davy Brouzet ◽  
Mohsen Talei ◽  
Robert L. Gordon ◽  
Quentin Cazeres ◽  
...  

Fluids ◽  
2019 ◽  
Vol 4 (3) ◽  
pp. 146 ◽  
Author(s):  
Aaron Endres ◽  
Thomas Sattelmayer

Boundary layer flashback from the combustion chamber into the premixing section is a threat associated with the premixed combustion of hydrogen-containing fuels in gas turbines. In this study, the effect of pressure on the confined flashback behaviour of hydrogen-air flames was investigated numerically. This was done by means of large eddy simulations with finite rate chemistry as well as detailed chemical kinetics and diffusion models at pressures between 0 . 5 and 3 . It was found that the flashback propensity increases with increasing pressure. The separation zone size and the turbulent flame speed at flashback conditions decrease with increasing pressure, which decreases flashback propensity. At the same time the quenching distance decreases with increasing pressure, which increases flashback propensity. It is not possible to predict the occurrence of boundary layer flashback based on the turbulent flame speed or the ratio of separation zone size to quenching distance alone. Instead the interaction of all effects has to be accounted for when modelling boundary layer flashback. It was further found that the pressure rise ahead of the flame cannot be approximated by one-dimensional analyses and that the assumptions of the boundary layer theory are not satisfied during confined boundary layer flashback.


AIAA Journal ◽  
1984 ◽  
Vol 22 (3) ◽  
pp. 388-393 ◽  
Author(s):  
Krishnan Radhakrishnan ◽  
David T. Pratt

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