First principles simulation of reacting hypersonic flow over a blunt wedge

被引:8
|
作者
Grover, Maninder S. [1 ,2 ]
Verhoff, Ashley M. [2 ]
Valentini, Paolo [1 ,2 ]
Bisek, Nicholas J. [2 ]
机构
[1] Univ Dayton, Res Inst, 1700 S Patterson Blvd, Dayton, OH 45409 USA
[2] US Air Force, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
CHEMICAL-KINETIC PROBLEMS; FUTURE NASA MISSIONS; DISSOCIATION; ENERGY;
D O I
10.1063/5.0161570
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This article presents molecular-level analysis of a reactive, near-continuum, Mach 21 nitrogen flow over a blunt wedge using the direct molecular simulation (DMS) method. The flow conditions lead to internal energy excitation and dissociation in the flow field, resulting in thermal and chemical nonequilibrium in the flow. Thermal nonequilibrium in the vibrational mode is observed to extend to the molecular level, where the vibrational energy distributions at various points in the flow field are observed to be non-Boltzmann. Furthermore, this is the first reactive DMS calculation where the wall is assumed to be isothermal and full momentum accommodation of the particles is enforced, hence incorporating viscous wall effects. Since the DMS method uses a quantum mechanically generated interaction potential as its only modeling input, all thermochemical and transport properties of the flow field can directly be attributed to the ab initio potential energy surface. Using the DMS solution as a benchmark, this article assesses the performance of Navier-Stokes computational fluid dynamics solutions using lower fidelity two-temperature models. Two models are chosen as points of comparison: the well-known Park two-temperature model and the recently developed modified Marrone and Treanor model.
引用
收藏
页数:17
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