Publication:
Возможности уточнения модели аэродинамики носовой полости

dc.contributor.authorИбрагим Юнус Абделхамид
dc.contributor.authorНосова, Я. В.
dc.contributor.authorАврунін, О. Г.
dc.date.accessioned2019-05-13T19:05:21Z
dc.date.available2019-05-13T19:05:21Z
dc.date.issued2019
dc.description.abstractThe 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.uk_UA
dc.identifier.citationИбрагим Юнусс Абделхамид Возможности уточнения модели аэродинамики носовой полости / Абделхамид Ибрахим Юнусс, Я. В. Носова, О. Г. Аврунин // Матеріали 23 Міжнародного молодіжного форуму. Т. 1. – Харків: ХНУРЕ. 2019. – С. 245 - 246uk_UA
dc.identifier.urihttp://openarchive.nure.ua/handle/document/8627
dc.language.isoruuk_UA
dc.publisherХНУРЕuk_UA
dc.subjectвозможности уточненияuk_UA
dc.subjectполость носоваяuk_UA
dc.titleВозможности уточнения модели аэродинамики носовой полостиuk_UA
dc.typeThesisuk_UA
dspace.entity.typePublication

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