基于飞参的尾翼载荷谱编制的均值法

Mean Method for Compiling Tail Load Spectrum Based on Flight Parameters

介绍了基于飞参的尾翼载荷谱编制的均值法,通过对飞参数据的处理获取尾翼载荷谱数据,用均值法编制飞机尾翼载荷谱。此方法编制的尾翼载荷谱可以为飞机尾翼的寿命分析和试验提供载荷谱依据。

The paper introduces the mean method for compiling tail load spectrum based on flight parameters.The tail load spectrum is obtained by processing flight parameter data and the mean method is used to compile the aircraft tail load spectrum.The tail load spectrum compiled using this method can provide a load spectrum basis for life analysis and testing of aircraft tail.