自由流
楔形(几何)
非平衡态热力学
振动温度
材料科学
机械
振动能量弛豫
红外线的
热力学
激发
物理
光学
湍流
原子物理学
雷诺数
激发态
量子力学
作者
Sangdi Gu,Richard G. Morgan,Timothy J. McIntyre,Aaron M. Brandis
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:2021-09-25
卷期号:60 (3): 1283-1292
被引量:6
摘要
An experimental study of flows subjected to expanding conditions relevant to Mars entry is presented. A condition with a nominal velocity of was generated in the X2 expansion tunnel. Midwavelength infrared emission measurements of the 4.3 and bands were made over both a two-dimensional wedge model and for the freestream. Consistent results in the characterization of the freestream were obtained from pressure and spectroscopic measurements. The rotational and vibrational temperatures estimated in the wedge flow using the band were consistent with those estimated from the band. The difference between the translational–rotational temperature and the vibrational temperature was shown to be small in the freestream and expanding flow over the wedge model: less than 10%. Using vibrational relaxation rates tuned for postshock conditions, computational fluid dynamics simulations significantly overestimated the thermal nonequilibrium in the expanding flow, but not in the postshock (compressive) flow. This observation is consistent with past results for and CO, as well as at lower temperatures.
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