Abstract
Experimental work was conducted to investigate the flame stability limits of H2 + C3H8, H2 + C2H6 and H2 + CH4 jet flames by using a single jet diffusion burner with a nozzle diameter of 2 mm. The results of 400 experimental tests showed that the increment of hydrogen composition increases the stability limits of the hydrogen-hydrocarbon jet flames. Furthermore, the results also showed that H2 + C3H8 jet flames could be effectively lifted or blown out at a lower jet exit velocity than H2 + C2H6 and H2 + CH4 jet flames at similar H2 concentrations. In addition, it was observed that the H2 + CH4 jet flame exhibits the highest blowout velocity. It was also found that the stability limit of hydrogen-hydrocarbon jet flames starts to increase rapidly at hydrogen volumetric composition of 90% for H2 + C3H8, 85% for H2 + C2H6 and 70% for H2 + CH4.
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Abbreviations
- H2 :
-
Hydrogen
- CH4 :
-
Methane
- C2H6 :
-
Ethane
- C3H8 :
-
Propane
- NTP:
-
Normal temperature and pressure (20 °C and 101.3 kPa
- ρ:
-
Density (kg/m3)
- \(\overline{\rho }\) :
-
The density ratio of the gas at the jet exit ρe to the density of the ambient air c
- ρe :
-
The density of the exiting fluid at 298 K (kg/m3)
- ρ∞ :
-
The density of the ambient air at 298 K (kg/m3
- C2 :
-
Constant which valued 50 (used in Eq. 1)
- do :
-
An inner diameter of the burner (mm)
- h:
-
Lift-off height (mm)
- Re H :
-
Reynolds number of the exit jet
- Re su :
-
The turbulence Reynolds number
- SL :
-
Laminar burning velocity (m/s)
- Ue :
-
Jet exit velocity (m/s)
- Ublowout :
-
Blow-out velocity (m/s)
- Ve :
-
The kinematic viscosity of the jet exit (m2/s)
- Vjet :
-
Viscosity (m2/s)
- XH2 :
-
Mole fraction of Hydrogen
- Yo :
-
Fuel mass fraction at the burner exit
- Ys :
-
Fuel fraction needed for stoichiometric burning
- Yst :
-
Stoichiometric mass fraction
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Acknowledgements
The authors would like to acknowledge the Ministry of Higher Education Malaysia (MOHE) for the financial support of this research. This research was supported by MOHE under the Fundamental Research Grant Scheme (FRGS) with the project code FP045-2020.
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Appendix
Appendix
This appendix shows the test conditions and experimental results (flame status) of 400 experimental tests on hydrogen and hydrocarbon jet flames. The flow rates, pressure, and flame status of each test were recorded, and the details are presented in Tables 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35.
Table 2 shows the test conditions and experimental results of pure hydrogen jet flames with a flow rate range from 10 to 150 L/min, while Tables 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13 and 14 show the test conditions and experimental results of hydrogen-methane jet flames with hydrogen flow rate varying from 10 to 120 L/min.
Tables 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25 and 26 show the test conditions and experimental results of hydrogen-ethane jet flames with different hydrogen flow rates from 10 to 110 L/min. Similarly, Tables 27, 28, 29, 30, 31, 32, 33, 34, 35 show the test conditions and experimental results of hydrogen-propane jet flames with a hydrogen flow rate varying from 10 to 100 L/min.
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Messaoudani, Z.l., Hamid, M.D., Wu, Y. et al. Experimental investigation of the flame stability limits for H2 + C3H8, H2 + C2H6 and H2 + CH4 jet flames. Braz. J. Chem. Eng. 39, 487–510 (2022). https://doi.org/10.1007/s43153-021-00169-4
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DOI: https://doi.org/10.1007/s43153-021-00169-4