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Brass instruments: Linear stability analysis and experiments with an artificial mouth

机译:黄铜仪器:线性稳定性分析和人工嘴实验

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摘要

The self-sustained oscillation of a brass wind musical instrument involves a complex aerodynamic coupling between multimode mechanical vibratory system (the Lips of the player) and a multimode acoustical vibratory system (the air column of the instrument). In this paper the behaviour of the coupled system near the threshold of oscillation is investigated using a simplified model in which a single mechanical lip mode is coupled to a single mode of the acoustical resonator. Linear stability analysis is used to study the theoretical variation of threshold blowing pressure and threshold playing frequency as functions of lip and air column parameters. The theoretical results are compared with experimental results obtained from a systematic study of the near threshold behaviour of a trombone sounded by an artificial lip mechanism. Comparability between theory and experiment is ensured by using model parameter values derived from mechanical response measurements on the artificial lips and input impedance measurements on the trombone. The measured mechanical response curve for the artificial lips exhibits several resonance peaks, each of which can be classified unambiguously as either "inward striking" or "outward striking". For each of these resonance peaks, parameters have been extracted and used in numerical simulation of threshold behaviour as a function of trombone slide extension. However, the experimentally observed threshold frequencies of the coupled system suggest a behaviour which passes smoothly from "inward striking" to "outward striking" character as the trombone slide is extended or the embouchure parameters changed. It seems unlikely that this type of behaviour can be explained using a lip model with only a single degree of freedom. [References: 49]
机译:铜管乐器的自持振荡涉及多模式机械振动系统(演奏者的嘴唇)和多模式声学振动系统(乐器的气柱)之间的复杂气动耦合。在本文中,使用简化模型研究了耦合系统在振荡阈值附近的行为,在该简化模型中,单个机械唇形模式耦合到声学谐振器的单个模式。线性稳定性分析用于研究阈值吹气压力和阈值演奏频率作为唇形和气柱参数的函数的理论变化。理论结果与实验结果进行了比较,实验结果是通过对人工嘴唇机制发出的长号的接近阈值行为进行系统研究而获得的。通过使用模型参数值来确保理论和实验之间的可比性,这些模型参数值是从人造唇上的机械响应测量值和长号上的输入阻抗测量值得出的。所测量的人造嘴唇的机械响应曲线表现出几个共振峰,每个共振峰都可以明确地分类为“向内撞击”或“向外撞击”。对于这些共振峰中的每个共振峰,已经提取了参数并将其用于阈值行为的数值模拟,作为长号滑动扩展的函数。但是,实验观察到的耦合系统的阈值频率表明,随着长号滑动片的伸展或包囊参数的变化,该行为会从“向内”平稳过渡到“向外”。使用仅具有单个自由度的嘴唇模型无法解释这种行为。 [参考:49]

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