COMPOSITE COOLING OF PERFORATED PLATES IN TURBULENT GAS FLOW
- Author
- GLAZKOV VV; GUSEV MD; ZHESTOV BA
INST. AIRCRAFT ENGINES,MOSCOW,SUN - Source
- HEAT TRANSFER, SOVIET RES.; USA; DA. 1978; VOL. 10; NO 5; PP. 57-62; BIBL. 6 REF.
- Document type
- Article
- Language
- English
- Keyword (fr)
- TRANSFERT CHALEUR MASSE COUCHE LIMITE PLAQUE PERFOREE REFROIDISSEMENT ETUDE EXPERIMENTALE COEFFICIENT TRANSFERT CHALEUR EQUATION ECOULEMENT TURBULENT GAZ TEMPERATURE ENERGIE MECANIQUE FLUIDE
- Keyword (en)
- HEAT MASS TRANSFER BOUNDARY LAYER PERFORATED PLATE COOLING EXPERIMENTAL STUDY HEAT TRANSFER COEFFICIENT EQUATION TURBULENT FLOW GASES TEMPERATURE ENERGY FLUID MECHANICS
- Keyword (es)
- ENERGIA MECANICA DELOS FLUIDOS
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Energy Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL8070053298
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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