Literature DB >> 16706587

Flow visualization and acoustic consequences of the air moving through a static model of the human larynx.

Bogdan R Kucinschi1, Ronald C Scherer, Kenneth J DeWitt, Terry T M Ng.   

Abstract

Flow visualization with smoke particles illuminated by a laser sheet was used to obtain a qualitative description of the air flow structures through a dynamically similar 7.5x symmetric static scale model of the human larynx (divergence angle of 10 deg, minimal diameter of 0.04 cm real life). The acoustic level downstream of the vocal folds was measured by using a condenser microphone. False vocal folds (FVFs) were included. In general, the glottal flow was laminar and bistable. The glottal jet curvature increased with flow rate and decreased with the presence of the FVFs. The glottal exit flow for the lowest flow rate showed a curved jet which remained laminar for all geometries. For the higher flow rates, the jet flow patterns exiting the glottis showed a laminar jet core, transitioning to vortical structures, and leading spatially to turbulent dissipation. This structure was shortened and tightened with an increase in flow rate. The narrow FVF gap lengthened the flow structure and reduced jet curvature via acceleration of the flow. These results suggest that laryngeal flow resistance and the complex jet flow structure exiting the glottis are highly affected by flow rate and the presence of the false vocal folds. Acoustic consequences are discussed in terms of the quadrupole- and dipole-type sound sources due to ordered flow structures.

Entities:  

Mesh:

Year:  2006        PMID: 16706587     DOI: 10.1115/1.2187042

Source DB:  PubMed          Journal:  J Biomech Eng        ISSN: 0148-0731            Impact factor:   2.097


  18 in total

1.  Time-Dependent Pressure and Flow Behavior of a Self-oscillating Laryngeal Model With Ventricular Folds.

Authors:  Fariborz Alipour; Ronald C Scherer
Journal:  J Voice       Date:  2015-04-11       Impact factor: 2.009

2.  Computational study of false vocal folds effects on unsteady airflows through static models of the human larynx.

Authors:  Charles Farbos de Luzan; Jie Chen; Mihai Mihaescu; Sid M Khosla; Ephraim Gutmark
Journal:  J Biomech       Date:  2015-03-19       Impact factor: 2.712

3.  Using particle imaging velocimetry to measure anterior-posterior velocity gradients in the excised canine larynx model.

Authors:  Sid Khosla; Shanmugam Murugappan; Raghavaraju Lakhamraju; Ephraim Gutmark
Journal:  Ann Otol Rhinol Laryngol       Date:  2008-02       Impact factor: 1.547

4.  Influence of flow separation location on phonation onset.

Authors:  Zhaoyan Zhang
Journal:  J Acoust Soc Am       Date:  2008-09       Impact factor: 1.840

5.  Pressure distributions in a static physical model of the hemilarynx: measurements and computations.

Authors:  Lewis P Fulcher; Ronald C Scherer; Kenneth J De Witt; Pushkal Thapa; Yang Bo; Bogdan R Kucinschi
Journal:  J Voice       Date:  2008-06-06       Impact factor: 2.009

6.  A numerical and experimental investigation of the effect of false vocal fold geometry on glottal flow.

Authors:  Mehrdad H Farahani; John Mousel; Fariborz Alipour; Sarah Vigmostad
Journal:  J Biomech Eng       Date:  2013-12       Impact factor: 2.097

7.  Ventricular pressures in phonating excised larynges.

Authors:  Fariborz Alipour; Ronald C Scherer
Journal:  J Acoust Soc Am       Date:  2012-08       Impact factor: 1.840

8.  Unsteady laryngeal airflow simulations of the intra-glottal vortical structures.

Authors:  Mihai Mihaescu; Sid M Khosla; Shanmugam Murugappan; Ephraim J Gutmark
Journal:  J Acoust Soc Am       Date:  2010-01       Impact factor: 1.840

9.  Aerodynamic and acoustic effects of ventricular gap.

Authors:  Fariborz Alipour; Michael Karnell
Journal:  J Voice       Date:  2013-12-08       Impact factor: 2.009

10.  A computational study of the effect of false vocal folds on glottal flow and vocal fold vibration during phonation.

Authors:  Xudong Zheng; Steve Bielamowicz; Haoxiang Luo; Rajat Mittal
Journal:  Ann Biomed Eng       Date:  2009-01-14       Impact factor: 3.934

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