TY - GEN
T1 - Simulation of radiation generated by chemical reactions in weakly ionized shock waves using DSMC
AU - Zhu, Tong
AU - Liy, Zheng
AU - Levinz, Deborah A.
PY - 2014
Y1 - 2014
N2 - In this work, we simulate the radiation from the NO and N+ 2 systems and compare with the shock tube experiments in air by Gorelov.1 The related shock speeds are high enough to have produced a peak translational temperature of ~20,000 K or even higher, providing enough energy to ionize some of the flow species. In the current work, we simulate ionized normal shock flows by implementing appropriate ionization models in a 11 species air (N, O, N2, O2, NO, N+, O+, N+ 2, O+ 2, NO+ and e-) in DSMC. Electron impact and heavy particle impact excitation for NO is studied using the Quasi-Steady-State (QSS) approximation to compute the NO(A2IeΣ+u) and the N+ 2 (B2IeΣ+ u) state number densities. Line-by-line calculation of the spectra is performed using the NEQAIR2 code to obtain radiation in the wavelength range of 235 ± 7 and 391:4 ± 0:2 nm. For shock speeds above 7 km/s, the currently calculated radiation are in better agreement with the experimental data than that in our eariler work,3 but are still about 2~6 times lower than the experiments. For the N+ 2 radiation good agreement with the experimental data is obtained for shock speeds above 9 km/s.
AB - In this work, we simulate the radiation from the NO and N+ 2 systems and compare with the shock tube experiments in air by Gorelov.1 The related shock speeds are high enough to have produced a peak translational temperature of ~20,000 K or even higher, providing enough energy to ionize some of the flow species. In the current work, we simulate ionized normal shock flows by implementing appropriate ionization models in a 11 species air (N, O, N2, O2, NO, N+, O+, N+ 2, O+ 2, NO+ and e-) in DSMC. Electron impact and heavy particle impact excitation for NO is studied using the Quasi-Steady-State (QSS) approximation to compute the NO(A2IeΣ+u) and the N+ 2 (B2IeΣ+ u) state number densities. Line-by-line calculation of the spectra is performed using the NEQAIR2 code to obtain radiation in the wavelength range of 235 ± 7 and 391:4 ± 0:2 nm. For shock speeds above 7 km/s, the currently calculated radiation are in better agreement with the experimental data than that in our eariler work,3 but are still about 2~6 times lower than the experiments. For the N+ 2 radiation good agreement with the experimental data is obtained for shock speeds above 9 km/s.
UR - http://www.scopus.com/inward/record.url?scp=84902806044&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84902806044&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84902806044
SN - 9781624102561
T3 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
BT - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
Y2 - 13 January 2014 through 17 January 2014
ER -