直升机传热与红外特征建模与分析(英文)

直升机蒙皮表面及排气温度分布受到发动机排气系统、旋翼下洗气流和太阳辐射的直接影响。为了能够精确地模拟直升机蒙皮表面及排气温度分布,在进行处于悬停状态的直升机三维流场和温度场建模与分析时,综合考虑了旋翼下洗对喷流的影响和太阳辐射对机身加热的影响。基于温度场和流场数据,通过正反射线踪迹法对直升机红外波段辐射强度的分布进行计算。针对一假想的排气系统与后机身融合的直升机模型,本文对其热特性和红外辐射特性进行了数值计算和分析。

Modeling and Analysis of Helicopter Thermal and Infrared Radiation

The temperature distributions on the helicopter airframe and in the exhaust plume are affected seriously by the engine exhaust system, rotor downwash and solar irradiance. To precisely simulate temperature distribution on the helicopter airframe and in the exhaust plume, the effects of rotor downwash and solar irradiance are considered in three-dimensional flow and heat transfer calculation under helicopter hovering. Based on the temperature distribution, a forward-backward ray tracing method is used to cal...