TY - JOUR
T1 - Effects of pressure and precursor loading in the flame synthesis of titania nanoparticles
AU - Zhao, Hong
AU - Liu, Xiaofei
AU - Tse, Stephen D.
N1 - Funding Information:
This work was supported mainly by the National Science Foundation through Grants NSF-CTS-0213929 and NSF-CTS-0325057 and partially by the Office of Naval Research through Grant N00014-08-1-1029. Special thanks are due to Mr. Joshua Dewanaga, Mr. Venkata Rapaka, Mr. Fusheng Xu, and Mr. John Petrowski for their help with the experiments.
PY - 2009/11
Y1 - 2009/11
N2 - The synthesis of TiO2 nanoparticles is investigated experimentally and computationally in low-pressure H2/O2/N2 burner-stabilized flat stagnation flames, using titanium tetra-iso-propoxide as precursor. The flow field is modeled with detailed chemical kinetics and transport, and is compared with measurements using laser-induced fluorescence to map gas-phase temperature and OH-radical species concentration. A sectional model, coupled with the simulated flow field and flame structure, is employed to model particle growth dynamics, computing aggregate particle size distribution, geometric standard deviation, and average primary particle size. The computations are compared with the experiments, for which in situ characterization of the nanoparticles in the flow field is accomplished by a low-pressure aerosol sampling system connected to a nano-scanning mobility particle sizer. Effects of operating pressure and precursor-loading rate on particle growth are examined experimentally and are compared with computational modeling. Different from other works, temperature profiles, rather than mass flow rate, are fixed using strategic dilution to base the comparisons. Higher pressures produce larger aggregate particles, but also smaller primary particles, due to longer residence times, as seen in both the experiments and computations. For higher precursor-loading rates, aggregate particle size is larger (for both experiments and computations), while primary particle size remains constant for the experiments and decreases slightly for the computations in the corresponding range.
AB - The synthesis of TiO2 nanoparticles is investigated experimentally and computationally in low-pressure H2/O2/N2 burner-stabilized flat stagnation flames, using titanium tetra-iso-propoxide as precursor. The flow field is modeled with detailed chemical kinetics and transport, and is compared with measurements using laser-induced fluorescence to map gas-phase temperature and OH-radical species concentration. A sectional model, coupled with the simulated flow field and flame structure, is employed to model particle growth dynamics, computing aggregate particle size distribution, geometric standard deviation, and average primary particle size. The computations are compared with the experiments, for which in situ characterization of the nanoparticles in the flow field is accomplished by a low-pressure aerosol sampling system connected to a nano-scanning mobility particle sizer. Effects of operating pressure and precursor-loading rate on particle growth are examined experimentally and are compared with computational modeling. Different from other works, temperature profiles, rather than mass flow rate, are fixed using strategic dilution to base the comparisons. Higher pressures produce larger aggregate particles, but also smaller primary particles, due to longer residence times, as seen in both the experiments and computations. For higher precursor-loading rates, aggregate particle size is larger (for both experiments and computations), while primary particle size remains constant for the experiments and decreases slightly for the computations in the corresponding range.
KW - Laser-induced fluorescence
KW - Nano-scanning mobility particle sizer
KW - Nanoparticles
KW - Precursor
KW - Pressure
KW - Residence time
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U2 - 10.1016/j.jaerosci.2009.07.004
DO - 10.1016/j.jaerosci.2009.07.004
M3 - Article
AN - SCOPUS:70350341711
SN - 0021-8502
VL - 40
SP - 919
EP - 937
JO - Journal of Aerosol Science
JF - Journal of Aerosol Science
IS - 11
ER -