Combustion analysis of a stratified pre-chamber ignition system by means of a zero-dimensional turbulence and flame speed model

2021 ◽  
Vol 232 ◽  
pp. 111526
Author(s):  
V. Macián ◽  
F.J. Salvador ◽  
J. De la Morena ◽  
V. Pagano
2019 ◽  
Vol 160 ◽  
pp. 113985 ◽  
Author(s):  
Nathália Duarte Souza Alvarenga Santos ◽  
Carlos Eduardo Castilla Alvarez ◽  
Vinícius Rückert Roso ◽  
José Guilherme Coelho Baeta ◽  
Ramon Molina Valle

Author(s):  
Philip Diwakar ◽  
Jaleel Valappil

This paper examines safety concerns related to flame speeds when warm relief gas snuffs out the pilot at the flare stack and pulls in ambient air and a spark ignites the vapor in the header. The flame speed essentially determines if the propagating flame speed is a deflagration or a detonation based on whether its subsonic or supersonic. While pipes are sized for deflagrations, they need to be analyzed and tested for detonation pressures and temperatures. Transient CFD calculations help determine the flame speeds, deflagration to detonation transition, pressures and temperatures are compared to pipe specifications and help determine if a detonation leads to a Loss of Containment and suggests mitigations.


2021 ◽  
Vol 33 (2) ◽  
pp. 025104
Author(s):  
Xin Wang ◽  
Xiaobei Cheng ◽  
Hao Lu ◽  
Yishu Xu ◽  
Yang Liu ◽  
...  

Author(s):  
Milan Sebok ◽  
Matej Kubis ◽  
Miroslav Gutten ◽  
Matej Kucera ◽  
Tomasz N. Koltunowicz ◽  
...  

ACS Omega ◽  
2021 ◽  
Vol 6 (35) ◽  
pp. 22848-22856
Author(s):  
Tessy S. Ritchie ◽  
Kathleen E. Riegner ◽  
Robert J. Seals ◽  
Clifford J. Rogers ◽  
Dawn E. Riegner
Keyword(s):  

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.


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