Возможности уточнения модели аэродинамики носовой полости

Abstract

The nasal cavity aerodynamic resistance, which takes into account both the loss in length and local resistances, is proposed. The equivalent pneumatic scheme of such a system may consist of parallel-connected aerodynamic resistances of conventionally divided common, lower, middle and upper nasal passages for each half of the nose. In addition, each nasal passage can be divided along the length into sections, which can be represented by equivalent aerodynamic series resistances.