Mathematical modeling of coupled heat transfer on cooled gas turbine blades

The paper presents a physico-mathematical model for determining the heat transfer parameters between viscous gasdynamic flotations and cooled gas turbine blades made using the technology of composite permeable membranes (CPM). The mathematical model includes equations of dynamic and thermal boundary...

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Detalhes bibliográficos
Main Authors: Ying SUN, Sergey A. KOLESNIK, Ekaterina L. KUZNETSOVA
Formato: Artigo
Idioma:Inglês
Publicado em: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2020-07-01
Colecção:INCAS Bulletin
Assuntos:
composite permeable membranes
gasdynamic flotation
cooling efficiency
software package
boundary layer
Acesso em linha:https://bulletin.incas.ro/files/sun_kolesnik_kuznetsova-ek-l__vol_12_special_issue.pdf
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