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Instationäre Grenzschichteffekte an Tragflügelprofilen

Other title
Unsteady boundary layer effects on airfoil sections (en)
Author
KRÜGER, S
Flensburger Schiffbau Ges., 24939 Flensburg, Germany
Source

Archive of applied mechanics (1991). = Ingenieur-Archiv (1991). 1994, Vol 64, Num 5, pp 317-345 ; ref : 21 ref

ISSN
0939-1533
Scientific domain
Civil engineering; Mechanical engineering; Mechanics acoustics
Publisher
Springer, Berlin
Publication country
Germany
Document type
Article
Language
German
Keyword (fr)
Décollement couche limite Décollement laminaire Instabilité Modèle prévision Profil aérodynamique Régime transitoire Transition
Keyword (en)
Boundary layer separation Laminar separation Instability Forecast model Airfoils Unsteady state Transition
Keyword (es)
Despegadura capa límite Despegadura laminar Modelo previsión Régimen transitorio Transición
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
4135014

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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