An experimental study on the instability of RP-3 aviation kerosene/air premixed flame
•This paper focused on the instability of RP-3 aviation kerosene/air premixed flame.•Experiments were carried out in a constant volume chamber to study the unstable flame propagation processes of RP-3/air premixed flame over wide initial conditions.•The transition acceleration onset was measured and...
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Published in | Fuel (Guildford) Vol. 332; p. 126038 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
15.01.2023
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Subjects | |
Online Access | Get full text |
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Summary: | •This paper focused on the instability of RP-3 aviation kerosene/air premixed flame.•Experiments were carried out in a constant volume chamber to study the unstable flame propagation processes of RP-3/air premixed flame over wide initial conditions.•The transition acceleration onset was measured and the effects of diffusional-thermal, hydrodynamic instability and stretch rate in spherically expanding flames on Rcr were analyzed.•The acceleration exponent α was obtaind and with the increase of equivalence ratio, the changes in α and its corresponding flame radius were analyzed.
In the present work, experiments were carried out in a constant volume chamber to study the unstable flame propagation processes of RP-3/air premixed flame at initial pressures of 0.1, 0.2 and 0.3 MPa, initial temperatures of 420, 450 and 480 K and over a wide equivalence ratio range from 1.0 to 1.7. Results show that the RP-3/air premixed flame tends to be unstable with increased equivalence ratio and initial pressure. The measured transition acceleration onset and calculated critical flame radius Rcr agree well with each other. The effects of diffusional- thermal, hydrodynamic instability and stretch rate in spherically expanding flames on α show that α of RP-3/air premixed flame strongly depends on effective Lewis number Leeff and Markstein number Ma. With the increase of equivalence ratio, acceleration exponent α tends to increase and the flame radius corresponding to the onset of similarity acceleration decreases. |
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ISSN: | 0016-2361 1873-7153 |
DOI: | 10.1016/j.fuel.2022.126038 |