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呼气气流受限中的室壁运动:梗阻与扑动。

Wall motion in expiratory flow limitation: choke and flutter.

作者信息

Webster P M, Sawatzky R P, Hoffstein V, Leblanc R, Hinchey M J, Sullivan P A

出版信息

J Appl Physiol (1985). 1985 Oct;59(4):1304-12. doi: 10.1152/jappl.1985.59.4.1304.

Abstract

Limitation of expiratory airflow from mammalian airways is currently understood to be due to choking at wave speed (S. V. Dawson and E. A. Elliott. J. Appl. Physiol. 43: 498-515, 1977). A critical weakness of the theory is the lack of a mechanism for the dissipation of energy when effort exceeds that needed for maximal flow. We have observed substantial wall motion with flow limitation in a physical model of a trachea. Therefore we have examined a simple two-dimensional mathematical model, designed to approximate the behavior of the physical model of the trachea, to try to identify a relationship between flow limitation and wall oscillation. The model matches wave-speed predictions when only long waves are considered. The model predicts that aerodynamic flutter will occur in the zone of supercritical flow described in wave-speed theory. Aerodynamic flutter in the zone of supercritical flow provides a potential mechanism for the energy dissipation necessary for transition from supercritical to subcritical flow and explains the high-frequency pure tone heard with flow limitation.

摘要

目前认为,哺乳动物气道呼气气流受限是由于在波速时出现阻塞(S. V. 道森和E. A. 埃利奥特,《应用生理学杂志》43: 498 - 515, 1977)。该理论的一个关键缺陷是,当用力超过最大流量所需的力时,缺乏能量耗散机制。我们在气管物理模型中观察到气流受限时有明显的管壁运动。因此,我们研究了一个简单的二维数学模型,旨在近似气管物理模型的行为,试图确定气流受限与管壁振荡之间的关系。当只考虑长波时,该模型与波速预测相符。该模型预测,在波速理论中描述的超临界流区域会发生气动颤振。超临界流区域的气动颤振为从超临界流转变为亚临界流所需的能量耗散提供了一种潜在机制,并解释了气流受限时听到的高频纯音。

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