Effect of source-tract acoustical coupling on the oscillation onset of the vocal folds

被引:33
作者
Lucero, Jorge C. [1 ]
Lourenco, Kelem G. [2 ]
Hermant, Nicolas [3 ]
Van Hirtum, Annemie [3 ]
Pelorson, Xavier [3 ]
机构
[1] Univ Brasilia, Dept Comp Sci, BR-70910900 Brasilia, DF, Brazil
[2] Univ Brasilia, Dept Math, BR-70910900 Brasilia, DF, Brazil
[3] Grenoble Univ, GIPSA Lab, CNRS, UMR 5216, F-38402 St Martin Dheres, France
关键词
acoustic resonance; biological tissues; speech processing; REGISTER TRANSITIONS; VOICE INSTABILITIES; THEORETICAL-MODELS; PHONATION; PRESSURE; FREQUENCY; BIRDSONG;
D O I
10.1121/1.4728170
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This paper analyzes the interaction between the vocal folds and vocal tract at phonation onset due to the acoustical coupling between both systems. Data collected from a mechanical replica of the vocal folds show that changes in vocal tract length induce fluctuations in the oscillation threshold values of both subglottal pressure and frequency. Frequency jumps and maxima of the threshold pressure occur when the oscillation frequency is slightly above a vocal tract resonance. Both the downstream and upstream vocal tracts may produce those same effects. A simple mathematical model is next proposed, based on a lumped description of tissue mechanics, quasi-steady flow and one-dimensional acoustics. The model shows that the frequency jumps are produced by saddle-node bifurcations between limit cycles forming a classical pattern of a cusp catastrophe. The transition from a low frequency oscillation to a high frequency one may be achieved through two different paths: in case of a large acoustical coupling (narrow vocal tract) or high subglottal pressure, the bifurcations are crossed, which causes a frequency jump with a hysteresis loop. By reducing the acoustical coupling (wide vocal tract) or the subglottal pressure, a path around the bifurcations may be followed with a smooth frequency variation. (C) 2012 Acoustical Society of America. [http://dx.doi.org/10.1121/1.4728170]
引用
收藏
页码:403 / 411
页数:9
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