Figures (18)  Tables (2)
    • Figure 1. 

      Ignition delay times of OME1–4/air. Symbols are experimental data of OME1 from Jacobs et al.[18] and of OME2–4 from Cai et al.[26]. Lines denote results calculated with kinetic models.

    • Figure 2. 

      Laminar burning velocities of OME1–4/air. Symbols are experimental data of OME1–2 from Shrestha et al.[29], of OME3 from Sun et al.[23], and of OME4 from Richter et al.[47]. Lines denote results calculated with kinetic models.

    • Figure 3. 

      Species concentrations during the oxidation of OME1–4. Symbols are experimental data of OME1 from Sun et al.[5], of OME2 from Wang et al.[13], and of OME3 from Qiu et al.[46] measured in jet stirred reactors, as well as experimental data of OME4 from Gaiser et al.[11] measured in a flow reactor. Lines denote results calculated with kinetic models.

    • Figure 4. 

      Point-wise difference between model and data for the various combustion targets of OME1–4.

    • Figure 5. 

      Point-wise difference between model and data for the combustion of OME1–3.

    • Figure 6. 

      Ignition delay times of OME1/O2/Ar mixtures. Lines represent results calculated with the Li_2021[19] and Cai_2020[26] models. Symbols denote experimental data from Li et al.[19].

    • Figure 7. 

      Sensitivities of IDTs on elementary reactions for OME1/O2/Ar mixtures at 1,250 K, φ = 1.0, and p =1 atm, 4 atm, and 10 atm calculated using the (a) Li_2021[19], and (b) the Cai_2020[26] models.

    • Figure 8. 

      Reaction fluxes during the auto-ignition of OME1/O2/Ar mixtures at 10 atm, 1,250 K, φ = 1.0, and 20% fuel consumption calculated using the Li_2021[19] and Cai_2020[26] models.

    • Figure 9. 

      Comparison of rate constants of direct fuel decomposition reaction and fuel decomposition reactions via unimolecular H-atom transfer of OME1 taken from the Li_2021[19] and Cai_2020[26] models.

    • Figure 10. 

      Sensitivities of IDTs on elementary reactions for OME3/air mixtures at 20 bar, φ = 1.0, and T = 600, 850, and 1,200 K, calculated by using the Shrestha_2022[29] model.

    • Figure 11. 

      Reaction fluxes during the auto-ignition of OME3/air mixtures at 20 bar, φ = 1.0, T = 600, 850, and 1,200 K, and 20% fuel consumption calculated by using the Shrestha_2022[29] model.

    • Figure 12. 

      Sensitivities of LBVs on elementary reactions of OME1−4/air mixtures at 400 K, 1 atm, and φ = 0.6, 1.0, and 1.4 calculated by using the Cai_2020[26] model.

    • Figure 13. 

      Concentrations of (a) OME2, and (b) OME3 during their pyrolysis at 1 atm and τ = 2 s. Lines represent results calculated with the Shrestha_2022[29] model, Cai_2020[26] model, and He_2018[25] model. Symbols denote experimental data from Zhong et al.[10].

    • Figure 14. 

      Sensitivities of the mole fractions of OME2 and OME3 on elementary reactions during their pyrolysis at 1 atm, τ = 2 s, and 800 K calculated by using the Shrestha_2022[29] model.

    • Figure 15. 

      Species concentrations of OME1/O2/He mixture. Lines represent results calculated with the Li_2021[19] and Jacobs_2019[18] models. Symbols denote experimental data from Vermeire et al.[17] measured in a jet stirred reactor at p = 1.07 bar, φ = 1.0, and τ = 2.83 s.

    • Figure 16. 

      Sensitivities of the mole fractions of CH3OH on elementary reactions during the oxidation of OME1/O2/He mixture at p = 1.07 bar, φ = 1.0, and T = 650 and 880 K calculated by using the Li_2021[19] model.

    • Figure 17. 

      Comparison of calculated and measured mole fractions of CH3OH in the oxidation of OME1/O2/He mixture at p = 1.07 bar, φ = 1.0, and τ = 2.83 s. Lines represent results calculated with the Li_2021[19], Jacobs_2019[18], and modified Jacobs_2019[18] models. Symbols denote experimental data from Vermeire et al.[17].

    • Figure 18. 

      Comparison of rate constants of the reaction CH2OCH2OCH2O2H = trioxane + OH in the Li_2021[19] and Jacobs_2019[18] models.

    • Properties Facilities Conditions Ref.
      OME1 IDTs Shock tube OME1/O2/Ar, 1–10 atm, 1,000–1,500 K, φ = 0.5–2.0 [19]
      Shock tube OME1/air, 20–40 bar, 691–1213 K, φ = 1.0 [18]
      Rapid compression machine OME1/air, 10–40 bar, 590–688 K, φ = 1.0 [18]
      Flow reactor OME1/O2/N2, 1 atm, 651–697 K, φ = 1.0 [18]
      Shock tube OME1/air, 30 bar, 600–1,350 K, φ = 0.5–2.0 [7]
      Shock tube OME1/O2/Ar, 2–10 atm, 1,100–1,500 K, φ = 0.5–2.0 [4]
      Shock tube OME1/O2/N2, 1–16 bar, 1,100–1,750 K, φ = 1.0 [43]
      LBVs Combustion vessel OME1/air, 1–3 bar, 443 K, φ = 0.8–1.4 [29]
      Heat flux burner and combustion vessel OME1/air, 1–5 bar, 298–373 K, φ = 0.6–1.85 [22]
      Heat flux burner OME1/air, 1 bar, 393 K, φ = 0.6–1.9 [8]
      Bunsen burner OME1/air, 1–6 bar, 473 K, φ = 0.6–1.8 [43]
      CONCs Jet stirred reactor OME1/O2/Ar, 750 torr, 487–867 K, φ = 0.5 [44]
      Jet stirred reactor OME1/O2/N2, 10 atm, 450–1,200 K, φ = 0.2–1.5 [5]
      Jet stirred reactor OME1/He, 1.07 bar, 800–1,100 K (pyrolysis);
      OME1/O2/He, 1.07 bar, 500–1,100 K, φ = 0.25–2.0
      [17]
      Flow reactor OME1/O2/Ar, 1 atm, 750–1,250 K, φ = 0.8–2.0 [11]
      Jet stirred reactor OME1/O2/Ar, 1.0 atm, 500–1,100 K [45]
      Jet stirred reactor OME1/Ar, 1.03 atm, 450–1,080 K (pyrolysis) [10]
      Jet stirred reactor OME1/O2/He, 1.05 atm, 500–1,000 K, φ = 0.5–2.0 [13]
      OME2 IDTs Shock tube OME2/air, 10–20 bar, 663–1,112 K, φ = 0.5–2.0 [26]
      Shock tube OME2/O2/N2, 1–16 bar, 850–1,700 K, φ = 1.0 [12]
      Rapid compression machine OME2/air, 10–15 bar, 550–680 K, φ = 0.5–2.0 [29]
      Rapid compression machine OME2/air, 3–10 bar, 570–690 K, φ = 1.0 [6]
      Rapid compression machine OME2/air, 0.5–1 MPa, 600–715 K, φ = 0.5 [27]
      LBVs Combustion vessel OME2/air, 1–5 bar, 393–443 K, φ = 0. 6–1.9 [29]
      Heat flux burner OME2/air, 1 bar, 380–401 K, φ = 0. 6–1.9 [8]
      Bunsen burner OME2/air, 1–6 bar, 473 K, φ = 0.5–2.0 [12]
      CONCs Flow reactor OME2/He, 3.4 bar, 373–1,073 K (pyrolysis) [27]
      Flow reactor OME2/O2/Ar, 1 atm, 750–1,250 K, φ = 0.8–2.0 [11]
      Jet stirred reactor OME2/Ar, 1.03 atm, 450–1080 K (pyrolysis) [10]
      Jet stirred reactor OME2/O2/He, 1.05 atm, 500–1,000 K, φ = 0.5–2.0 [13]
      OME3 IDTs Shock tube OME3/air, 10–20 bar, 684–1,137 K, φ = 0.5–2.0 [26]
      Rapid compression machine OME3/air, 15 bar, 550–680 K, φ = 2.0; OME3/O2/CO2, 15 bar, 550–680 K, φ = 0.5 [29]
      Rapid compression machine OME3/air, 3–10 bar, 570–690 K, φ = 1.0 [6]
      LBVs Combustion vessel OME3/air, 1–3 bar, 393–443 K, φ = 0. 8–1.6 [29]
      Combustion vessel OME3/air, 1 atm, 408 K, φ = 0. 7–1.6 [23]
      Combustion vessel OME3/air, 1 atm, 363–423 K, φ = 0. 7–1.8 [9]
      CONCs Flow reactor OME3/O2/Ar, 1 atm, 750–1,250 K, φ = 0.8–2.0 [11]
      Jet stirred reactor OME3/O2/N2, 1 atm, 500–950 K, φ = 0.5–2.0 [46]
      Jet stirred reactor OME3/Ar, 1.03 atm, 450–1,080 K (pyrolysis) [10]
      Jet stirred reactor OME3/O2/He, 1.05 atm, 500–1,000 K, φ = 0.5–2.0 [13]
      OME4 IDTs Shock tube OME4/air, 10–20 bar, 684–1,137 K, φ = 1.0 [26]
      LBVs Bunsen burner OME4/air, 1–6 bar, 473 K, φ = 0.5–2.0 [47]
      CONCs Flow reactor OME4/O2/Ar, 1 atm, 750–1,250 K, φ = 0.8–2.0 [11]

      Table 1. 

      Summary of experimental studies on OME1−4 combustion.

    • Model Fuels No. of species No. of reactions Ref.
      Dinelli_2024 OME1−5 183 2,532 [31]
      De Ras_2023 OME1−2 376 3,988 [28]
      Shrestha_2022 OME1−3 259 1,678 [29]
      De Ras_2022 OME1−2 301 2,251 [27]
      Niu_2021 OME1−6 92 389 [30]
      Li_2021 OME1 121 646 [19]
      Cai_2020 OME1−4 322 1,612 [26]
      Jacobs_2019 OME1 530 2,901 [18]
      He_2018 OME1−3 225 1,082 [25]
      Vermeire_2018 OME1 351 2,904 [17]

      Table 2. 

      Summary of OMEs kinetic models.