Rating the perception of jet noise crackle

Paul B. Russavage, T. Neilsen, K. Gee, S. H. Swift
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引用次数: 5

Abstract

Crackle is a perceptual aspect of noise caused by impulsive acoustic shocks and observed in noise from supersonic jets, including those from military aircraft and rockets. Overall and long-term spectral noise metrics do not account for the unique perception of crackle. Listening tests were designed to better understand perception of crackle and examine its relationship to physical noise metrics, such as skewness of the first time derivative of the pressure waveform, hereafter derivative skewness. It is hypothesized that as derivative skewness increases, the perception of crackle tends to increase. Two listening tests were conducted with 31 subjects to examine their perception of crackle. In the first test, subjects compared and ordered crackle-containing sounds. In the second test, category scaling was employed with subjects rating the crackle content with category labels: 1) smooth noise with no crackle, 2) rough noise with no crackle, 3) sporadic or intermittent crackle, 4) continuous crackle, and 5) intense crackle. Both the order and rating tests confirm there is a high correlation between perception of crackle and derivative skewness. These insights will help inform community noise models, allowing them to incorporate annoyance due to jet crackle.Crackle is a perceptual aspect of noise caused by impulsive acoustic shocks and observed in noise from supersonic jets, including those from military aircraft and rockets. Overall and long-term spectral noise metrics do not account for the unique perception of crackle. Listening tests were designed to better understand perception of crackle and examine its relationship to physical noise metrics, such as skewness of the first time derivative of the pressure waveform, hereafter derivative skewness. It is hypothesized that as derivative skewness increases, the perception of crackle tends to increase. Two listening tests were conducted with 31 subjects to examine their perception of crackle. In the first test, subjects compared and ordered crackle-containing sounds. In the second test, category scaling was employed with subjects rating the crackle content with category labels: 1) smooth noise with no crackle, 2) rough noise with no crackle, 3) sporadic or intermittent crackle, 4) continuous crackle, and 5) in...
评定对喷射噪声噼啪声的感知
裂纹是由脉冲声冲击引起的噪声的感知方面,在超音速喷气机(包括军用飞机和火箭)的噪声中观察到。总体和长期的频谱噪声度量不能解释对裂纹的独特感知。设计听力测试是为了更好地理解对裂纹的感知,并检查其与物理噪声指标的关系,例如压力波形的第一次导数偏度,之后的导数偏度。假设随着导数偏度的增加,裂纹的感知倾向于增加。对31名受试者进行了两项听力测试,以考察他们对噼啪声的感知。在第一个测试中,受试者比较并排序含有噼啪声的声音。在第二个测试中,采用类别标度法,受试者用类别标签对裂纹内容进行评分:1)平滑噪声无裂纹,2)粗糙噪声无裂纹,3)零星或间歇性裂纹,4)连续裂纹,5)强烈裂纹。顺序和等级测试都证实,裂纹感知和导数偏度之间存在高度相关性。这些见解将有助于建立社区噪音模型,使他们能够将喷气机噼啪声引起的烦恼纳入其中。裂纹是由脉冲声冲击引起的噪声的感知方面,在超音速喷气机(包括军用飞机和火箭)的噪声中观察到。总体和长期的频谱噪声度量不能解释对裂纹的独特感知。设计听力测试是为了更好地理解对裂纹的感知,并检查其与物理噪声指标的关系,例如压力波形的第一次导数偏度,之后的导数偏度。假设随着导数偏度的增加,裂纹的感知倾向于增加。对31名受试者进行了两项听力测试,以考察他们对噼啪声的感知。在第一个测试中,受试者比较并排序含有噼啪声的声音。在第二个测试中,采用类别标度法,受试者用类别标签对裂纹内容进行评分:1)平滑噪声无裂纹,2)粗糙噪声无裂纹,3)零星或间歇性裂纹,4)连续裂纹,5)在…
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