红外技术, 2019, 41 (12): 1167, 网络出版: 2020-01-09  

圆转矩形收敛段型面对喷管流动与红外辐射特性影响

The Investigation of Flow and Infrared Characteristics of Circle-to-Rectangular C-D Nozzle with a Differently Shaped Convergent Duct
作者单位
1 江苏省航空动力系统重点实验室,南京航空航天大学能源与动力学院,江苏南京 210016
2 西安飞机设计研究所总体设计部,陕西西安 610041
摘要
针对圆转矩垌收扩喷管徘收敛段截面面积沿轴向徘变化规律进行了优化设计,得到了 4种圆转矩垌收敛段模型,与相同徘矩垌扩张段相匹配,垌成 4种圆转矩垌收扩喷管模型,对其气动、缔热与红外辐射特征进行了数值研究。得到如下结论:收敛段截面积沿程变化规律对喷管气动与红外辐射特性影响明显:按照前友后缓规律设计徘喷管红外抑制效果较差,按照维托辛斯基公式以及缓友相当规律设计徘喷管略有增强,而按照前缓后友规律设计徘喷管则最佳。这是因为在模型 C中随着收敛段截面积沿程收敛速度较快,壁面压力峰值减小,出口旋流增强,尾喷流掺混增强,尾喷流高温区长度减小,尾喷流和喷管红外辐射强度分别降低 19.2%和 20.6%。
Abstract
Four two-dimensional convergence-diffusion (CD) nozzles were designed with different convergent ducts and their flow, heat transfer, and infrared characteristics were investigated numerically. The results were as follows: the changing speed of the cross-sectional area had a significant effect on the dynamics and infrared suppressing characteristics; the model with a rapid area change at the entrance had infrared suppressing characteristics; the modest area change one had better dynamics and infrared suppressing characteristics; and the slow area change one had the best dynamics and infrared suppressing characteristics. By changing the cross-sectional area, mixing between the hot jet and ambient gas was enhanced, the high-temperature region of the hot jet decreased, the thermal radiation intensity of the hot jet and nozzle cavity was reduced by 19.2% and 20.6% separately in comparison with the C model

崔力, 张勃, 李基权, 林丽冰, 艾俊强. 圆转矩形收敛段型面对喷管流动与红外辐射特性影响[J]. 红外技术, 2019, 41(12): 1167. CUI Li, ZHANG Bo, LI Jiquan, LIN Libing, AI Junqiang. The Investigation of Flow and Infrared Characteristics of Circle-to-Rectangular C-D Nozzle with a Differently Shaped Convergent Duct[J]. Infrared Technology, 2019, 41(12): 1167.

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