TY - GEN
T1 - An experimental and theoretical investigation of femtosecond laser excitation in N2 + O2 mixtures
AU - Zhang, Yibin
AU - Shneider, Mikhail N.
AU - Miles, Richard B.
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Oxygen is found to have both a quenching and amplifying effect on Femtosecond Laser Electronic Excitation Tagging at different mixture fractions with nitrogen. The strongest signal is still achieved in a pure nitrogen gas flow. When oxygen is initially added, the total signal quickly decreases before increasing again to a local maximum level around 50% nitrogen + 50% oxygen, and then decreases as the relative amount of oxygen in the mixture continues to increase. No obvious changes in the first or second positive emission are observed to explain this effect. Experiments and modeling both suggest that long-lived secondary species, NO and O3, could be responsible for these effects. A zero-dimensional kinetics model is developed to study and explain the effects of oxygen on FLEET emission in mixtures of nitrogen and oxygen at atmospheric pressure and temperature.
AB - Oxygen is found to have both a quenching and amplifying effect on Femtosecond Laser Electronic Excitation Tagging at different mixture fractions with nitrogen. The strongest signal is still achieved in a pure nitrogen gas flow. When oxygen is initially added, the total signal quickly decreases before increasing again to a local maximum level around 50% nitrogen + 50% oxygen, and then decreases as the relative amount of oxygen in the mixture continues to increase. No obvious changes in the first or second positive emission are observed to explain this effect. Experiments and modeling both suggest that long-lived secondary species, NO and O3, could be responsible for these effects. A zero-dimensional kinetics model is developed to study and explain the effects of oxygen on FLEET emission in mixtures of nitrogen and oxygen at atmospheric pressure and temperature.
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U2 - 10.2514/6.2017-3899
DO - 10.2514/6.2017-3899
M3 - Conference contribution
AN - SCOPUS:85086688047
SN - 9781624105029
T3 - 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2017
BT - 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -