升力体缝隙模型红外测热试验及分析OA北大核心CSTPCD

The infrared thermal measurements and data analysis of a lifting-body model with gaps were carried out in the Φ0.3 m hypersonic low-density wind tunnel of China Aerodynamics Research and Development Center.The experimental Mach number is 12,the total temperature is 668 K,the total pressure is 4.731 MPa,and the attack angles are 0° and 35°.Infrared thermograms of the model were obtained through experiments,and corresponding numerical simulation analysis was conducted.On this basis,the influence of selecting different frames of the infrared thermograms for data processing on the heat flux results was studied,and the heat flux increment caused by the gap interference was also analyzed.The results show that model jitter has a significant impact on the data processing after model release,thus it is recommended to select the infrared thermography results after the model reaches the stable state(about 1.2 s)in the data processing.More attention needs to be paid to the heat flux increase in the interference area of the T-shaped gaps,especially at 35°angle of attack,where the peak heat flux in the interference area of the gaps can reach more than 8 times that of the non-gap condition.The infrared thermal measurement data is in good agreement with the CFD results,and some difference only appears in a small peak interference area.In the next stage,more work needs to be carried out in the CFD model chamfering and the infrared thermal measurement scheme optimization.