Unsteady behavior and thermochemical non equilibrium effects in hypersonic double-wedge flows

被引:22
|
作者
Ninni, Davide [1 ,2 ]
Bonelli, Francesco [1 ,2 ,4 ]
Colonna, Gianpiero [3 ]
Pascazio, Giuseppe [1 ,2 ]
机构
[1] Politecn Bari, DMMM, Via Re David 200, I-70125 Bari, Italy
[2] Politecn Bari, CEMeC, Via Re David 200, I-70125 Bari, Italy
[3] CNR ISTP, Via Amendola 122-D, I-70126 Bari, Italy
[4] von Karman Inst Fluid Dynam, Aeronaut & Aerosp Dept, B-1640 Rhode St Genese, Belgium
关键词
Hypersonic flows; Thermochemical non-equilibrium; Double-wedge; Shock wave/boundary layer interaction; Periodic flows; VIBRATIONAL KINETICS; BOUNDARY-LAYER; TRANSPORT; AIR; MODELS;
D O I
10.1016/j.actaastro.2021.10.040
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The paper presents highly detailed two-dimensional numerical simulations of hypersonic nitrogen and air flows around a double wedge, characterized by a complex shock wave/boundary layer interaction (SWBLI). The aim of the study is on one hand to investigate the unsteady behavior of such an interaction and on the other to evaluate thermo-chemical non-equilibrium effects. Two different thermo-physical models have been considered, the classical multi-temperature, or mode approximation, and the state-to-state vibrational kinetics. It is shown that for the geometric configuration under investigation, the occurrence of unsteady periodic behavior depends on the flow conditions and is inhibited in the high enthalpy case. Furthermore, non-equilibrium effects become relevant in the case of high enthalpy flows and discrepancies between the results obtained with the two models are observed.
引用
收藏
页码:178 / 192
页数:15
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