高温气体辐射发光下温敏涂层热流密度辨识方法
Method for Identifying Heat Flux of Temperature-Sensitive Paint under High-Temperature Gas Radiation
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摘要: 为解决温敏涂层技术在高温气体辐射发光等强干扰条件下的热流密度辨识难题, 基于涂层表面辐射光强的梯度变化, 采用 Levenberg-Marquardt 优化算法, 建立了气体辐射发光条件下全局最优化热流密度辨识方法。并采用平板-楔模型在高焓激波风洞中开展了实验研究, 实验来流总温分别为 2 816 K 与 4 620 K。结果表明:高温气体辐射对光学测量方法有重要影响, 随着来流总温的增加, 气体辐射发光进一步增强。涂层表面光强梯度幅值随时间逐渐降低, 并趋于稳定值; 在不同总温条件下, 温升较小的平板区域, 气体辐射光强梯度幅值在总梯度幅值中的最大占比为 16.9%, 在温升较大的区域占比在 4.8%以下。基于梯度变化的全局最优化热流密度辨识方法在气体辐射光强梯度占比较小的条件下可有效消除高温气体辐射发光的影响, 获得较为可靠的热流密度数据, 在平板无干扰区及楔面热流密度峰值区域与热电偶测量结果相差在 20%以内。Abstract: In order to solve the problem of heat flux identification of temperature-sensitive paints under the interference condition of high-temperature gas radiation luminescence, based on the gradient change of radiation light intensity of the coating, a heat flux identification method using the Levenberg-Marquardt optimization algorithm had been established, and experiments were carried out using the flat plate-wedge model in the high-enthalpy shock tunnel, with the total temperature of 2 816 K and 4 620 K, respectively. The results show that the high-temperature gas radiation has an important influence on the optical measurement method, and the gas radiation luminescence is further enhanced with the increase of the total temperature of the incoming flows. The amplitude of the light intensity gradient on the coating surface gradually decreases with time and tends to be stable. Under different total temperature conditions, in the flat area with a small temperature rise, the maximum value of the gas radiation light intensity gradient amplitude in the total gradient amplitude is 16.9%, accounting for less than 4.8% in areas with large temperature rise. The global optimal heat flux identification method based on gradient change can effectively eliminate the influence of high-temperature gas radiation, and the difference between the measurement results of temperature-sensitive paint and the thermocouple measurement results is less than 20% in the non-disturbing area of the plate and the peak heat flux area of the wedge.