飞行状态下辐射板强化尾喷流红外抑制效果的数值研究

Numerical Study on Infrared Suppression Effect Enhancement from Plume by Using Radiant Plate Under Flight Condition

  • 摘要: 飞行器尾后大角度以及侧向红外辐射日益成为敌方的探测目标,降低3~5 μm波段内尾喷流的红外辐射特征是提高对应波段内红外抑制效果的有效途径。本文研究了在轴对称收敛喷管内安装辐射板对降低尾喷流温度以及红外抑制的作用。本文在Ma=0.8条件下,研究了安装十字辐射板前后,喷管换热及红外辐射特征的变化。结果表明,引入辐射板可以缩短尾喷流高温区长度。Ma=0.8时,引入辐射板结构使得90°方向上尾喷流的红外辐射强度降低了11.31%。论文进一步从对流换热与热辐射的耦合作用角度对其进行了解释。

     

    Abstract: The large-angle and lateral infrared radiation behind the aircraft are increasingly becoming detection targets of the enemy. Reducing the infrared radiation characteristics of the plume in the 3–5 μm bands is an effective way to improve the infrared suppression effect within the corresponding range. In this study, the effects of installing a radiant plate in an axisymmetric convergent nozzle on reducing the plume temperature and suppressing infrared radiation were investigated. In this study, the changes in the heat transfer and infrared radiation characteristics of the nozzle were studied before and after installation of the cross-radiant plate under Ma=0.8. The results indicated that the introduction of a radiant plate can shorten the length of the high-temperature region of the plume. At Ma=0.8, the infrared radiation intensity of the plume in the 90° direction decreased by 11.31%. This study further explains this phenomenon from the perspective of the coupling effect of convective heat transfer and thermal radiation.

     

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