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 inFuel (Guildford) Vol. 332; p. 126038
Main Authors Liu, Yu, Rao, Dawei, Wang, Enqing, Ma, Hongan, Zheng, Weilin, Zeng, Wen
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 15.01.2023
Subjects
Acceleration exponent
Critical flame radius
Onset of similarity acceleration
RP-3/air premixed flame
Transition acceleration onset
RP-3/air premixed flame
Acceleration exponent
Onset of similarity acceleration
Transition acceleration onset
Critical flame radius
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Abstract •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.
AbstractList •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.
ArticleNumber 126038
Author Ma, Hongan
Rao, Dawei
Zeng, Wen
Liu, Yu
Wang, Enqing
Zheng, Weilin
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CitedBy_id crossref_primary_10_1016_j_fuel_2024_131185
crossref_primary_10_1016_j_ijhydene_2024_04_302
crossref_primary_10_3390_aerospace11020163
crossref_primary_10_1016_j_fuel_2023_127643
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Keywords RP-3/air premixed flame
Acceleration exponent
Onset of similarity acceleration
Transition acceleration onset
Critical flame radius
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  publication-title: Combust Sci Technol
  doi: 10.1080/00102208308923635
  contributor:
    fullname: Frankel
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Snippet •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...
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elsevier
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StartPage 126038
SubjectTerms Acceleration exponent
Critical flame radius
Onset of similarity acceleration
RP-3/air premixed flame
Transition acceleration onset
Title An experimental study on the instability of RP-3 aviation kerosene/air premixed flame
URI https://dx.doi.org/10.1016/j.fuel.2022.126038
Volume 332
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