Vibrational state-to-state and multiquantum effects for N2 + N2 interactions at high temperatures for aerothermodynamic applications

被引:0
作者
Grover, Maninder S. [1 ,3 ]
Valentini, Paolo [1 ,3 ]
Josyula, Eswar [1 ,4 ]
Chaudhry, Ross S. [2 ]
机构
[1] Air Force Res Lab, Wright Patterson AFB, OH 45433 USA
[2] Univ Michigan, Dept Aerosp Engn, 1320 Beal Ave, Ann Arbor, MI 48109 USA
[3] Univ Dayton, Res Inst, Dayton, OH 45469 USA
[4] AFRL RQHF, Wright Patterson AFB, OH USA
来源
AIAA SCITECH 2020 FORUM | 2020年
关键词
CHEMICAL-KINETIC PROBLEMS; FUTURE NASA MISSIONS; ENERGY TRANSFER; DISSOCIATION RATES; RATE COEFFICIENTS; ANALYTIC MODEL; NONEQUILIBRIUM; NITROGEN; FLOWS; N2;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper we study the vibrational energy transfer process and dissociation due to N-2 + N-2 collisions using the state-to-state method. We discuss vibrational state transition rates and vibrational state specific dissociation rates obtained from QCT using the PES developed at the University of Minnesota [1, 2]. We first simulate an isothermal heat bath without dissociation to study the vibrational energy transfer process in isolation and then investigate nonequilibrium dissociation under QSS conditions to examine the impact of state-transitions and state-specific dissociation rates in a coupled simulation. Lastly, this paper delineates the role of multiquantum effects on vibrational energy transfer and dissociation to establish an engineering criteria to limit multi quantum effects so as to make the state-to-state approach computationally feasible for realistic geometries. The analysis was carried out over a temperature range of T = 8000 K to 30000 K. The multi quantum truncation criteria proposed can reduce state-to-state computational cost up to similar to 65% at the low temperature end of T = 8000 K and up to similar to 12% at the high temperature end of T = 30000 K while being within 10% of the accuracy of the full vibrational state-to-state solution.
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页数:22
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