Simulation study on infrared radiation characteristics of jet nozzle of turbofan engine by lobe mixer

• Published in: AIP advances Vol. 14; no. 10
• Main Authors: Chen, Lihai, Lou, Zongyong, Li, Dawei, Qiao, Lei
• Format: Journal Article
• Language: English
• Published: 01.10.2024
• ISSN: 2158-3226; 2158-3226
• DOI: 10.1063/5.0223112

With the rapid development of infrared detection technology, the importance and urgency of air-craft infrared stealth are becoming increasingly prominent. The engine exhaust system is one of the main infrared radiation sources of fighter aircraft, and it is of great significance to effectively suppress the infrared radiation of the engine exhaust system and tail jet. In this paper, based on the Reverse Monte Carlo Method, a program is developed to calculate the infrared radiation characteristics of an aeroengine exhaust system and evaluate the infrared suppression effect. The Ray Tracing Method is created to search the control body that passes through the ray transmission path, and the computing efficiency is greatly improved. Based on the program, the effect of the lobe mixer on the infrared characteristics of the engine exhaust system is analyzed. The results show that the use of the lobe mixer can not only effectively suppress the gas radiation but also reduce the solid radiation intensity of the high temperature wall and play a good infrared suppression effect on all detection directions of the exhaust system.