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7
Dynamics of temporal variations in phonatory flow.发声气流时变动力学。
J Acoust Soc Am. 2010 Jul;128(1):372-83. doi: 10.1121/1.3365312.
8
Unsteady laryngeal airflow simulations of the intra-glottal vortical structures.声门内涡旋结构的不稳定喉气流模拟
J Acoust Soc Am. 2010 Jan;127(1):435-44. doi: 10.1121/1.3271276.
9
Unsteady behavior of flow in a scaled-up vocal folds model.放大的声带模型中流动的非稳定行为。
J Acoust Soc Am. 2007 Dec;122(6):3659-70. doi: 10.1121/1.2409485.

本文引用的文献

1
Flow separation in a computational oscillating vocal fold model.计算振荡声带模型中的流动分离
J Acoust Soc Am. 2004 Sep;116(3):1710-9. doi: 10.1121/1.1779274.
2
Influence of collision on the flow through in-vitro rigid models of the vocal folds.碰撞对通过声带体外刚性模型的气流的影响。
J Acoust Soc Am. 2003 Dec;114(6 Pt 1):3354-62. doi: 10.1121/1.1625933.
3
Unsteady flow through in-vitro models of the glottis.通过声门体外模型的非定常流动。
J Acoust Soc Am. 2003 Mar;113(3):1658-75. doi: 10.1121/1.1547459.
4
Experimental verification of the quasi-steady approximation for aerodynamic sound generation by pulsating jets in tubes.管内脉动射流气动声产生的准稳态近似的实验验证。
J Acoust Soc Am. 2002 Oct;112(4):1652-63. doi: 10.1121/1.1506159.
5
Characteristics of a pulsating jet through a small modulated orifice, with application to voice production.
J Acoust Soc Am. 1997 Aug;102(2 Pt 1):1121-33. doi: 10.1121/1.419864.
6
Voice simulation with a body-cover model of the vocal folds.使用声带的身体覆盖模型进行语音模拟。
J Acoust Soc Am. 1995 Feb;97(2):1249-60. doi: 10.1121/1.412234.
7
Computer model to characterize the air volume displaced by the vibrating vocal cords.
J Acoust Soc Am. 1978 May;63(5):1559-65.

发声过程中非定常空气动力学效应的理论评估。

Theoretical assessment of unsteady aerodynamic effects in phonation.

作者信息

Krane Michael H, Wei Timothy

机构信息

Center for Advanced Information Processing, Rutgers University, Piscataway, New Jersey 08854, USA.

出版信息

J Acoust Soc Am. 2006 Sep;120(3):1578-88. doi: 10.1121/1.2215408.

DOI:10.1121/1.2215408
PMID:17004480
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC6624051/
Abstract

This paper ranks the importance of unsteady aerodynamic mechanisms in glottal flow. Particular emphasis is given to separation point motion, acceleration of glottal airflow by vocal fold motion, and viscous blockage. How nondimensional parameters such as the Reynolds, Strouhal, and Womersley numbers help in this ranking is also addressed. An equation of motion is derived which includes terms explicitly describing the effects of interest, assuming (1) a symmetrical glottis, (2) zero pressure recovery downstream of the vocal folds, and (3) a quasisteady glottal jet. Estimating the order of magnitude of the terms in this equation, it is shown that the flow is characterized by two temporal regimes: (1) a flow initiation/shutoff regime where local unsteady acceleration and wall motion dominate, and (2) a "quasisteady" regime where the flow is dominated by convective acceleration. In the latter case, separation point motion and viscous blockage are shown to be out of phase with motion of the vocal folds, thereby impacting the shape of the glottal volume flow waveform. The analysis suggests that glottal flow may be considered quasisteady only insofar as traditional assumptions concerning glottal jet behavior can be confirmed.

摘要

本文对声门气流中非定常气动机制的重要性进行了排序。特别强调了分离点运动、声带运动引起的声门气流加速以及粘性阻塞。还讨论了诸如雷诺数、斯特劳哈尔数和沃默斯利数等无量纲参数在这种排序中的作用。在假设(1)声门对称、(2)声带下游压力恢复为零以及(3)声门射流为准稳态的情况下,推导了一个运动方程,该方程明确包含了描述相关效应的项。通过估计该方程中各项的量级,结果表明气流具有两种时间状态:(1)流动起始/关闭状态,此时局部非定常加速度和壁面运动起主导作用;(2)“准稳态”状态,此时流动由对流加速度主导。在后一种情况下,分离点运动和粘性阻塞与声带运动不同相,从而影响声门体积流量波形的形状。分析表明,只有在能够证实关于声门射流行为的传统假设时,声门气流才可以被认为是准稳态的。