Effect of Reynolds number on boundary layer development behind an expansion fan
- Author
- GOL'DFEL'D, M. A; LISENKOV, I. G
- Source
Fluid dynamics. 1991, Vol 26, Num 5, pp 670-676 ; ref : 12 ref
- ISSN
- 0015-4628
- Scientific domain
- Mechanics acoustics
- Publisher
- Consultants Bureau, New York, NY
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Coin compression Couche limite Distribution pression Détente Essai soufflerie Etude expérimentale Nombre Reynolds Transition laminaire turbulente
- Keyword (en)
- Compression corner Boundary layer Pressure distribution Gas expansion Wind tunnel test Experimental study Reynolds number Turbulent laminar transition
- Keyword (es)
- Chareta compresión Capa límite Distribución presión Expansión gas Ensayo túnel aerodinámico Estudio experimental Número Reynolds Transición laminar turbulenta
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G40 Compressible flows; shock and detonation phenomena
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 5287754
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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DOI
10.1007/BF01050985 
https://dx.doi.org/10.1007/BF01050985
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