Unit-Reynolds-number effects on boundary-layer transition
- Author
- STETSON, K. F; KIMMEL, R. L
Wright-Pattern Air Force Base, Wright lab., high speed aero performance branch, United States - Source
AIAA journal. 1993, Vol 31, Num 1, pp 195-196 ; ref : 11 ref
- CODEN
- AIAJAH
- ISSN
- 0001-1452
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Article synthèse Couche limite transition Essai soufflerie Nombre Mach Nombre Reynolds Stabilité Transition laminaire turbulente
- Keyword (en)
- Review Transition boundary layer Wind tunnel test Mach number Reynolds number Stability Turbulent laminar transition
- Keyword (es)
- Artículo síntesis Capa límite transición Ensayo túnel aerodinámico Número Mach Número Reynolds Estabilidad Transición laminar turbulenta
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G20 Hydrodynamic stability
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 4529436
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
10.2514/3.11337 
https://dx.doi.org/10.2514/3.11337
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