The effect of 3D surface mounted obstacles on laminar, incompressible marginally separated boundary layer flows (Q2777690)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: The effect of 3D surface mounted obstacles on laminar, incompressible marginally separated boundary layer flows |
scientific article; zbMATH DE number 1717583
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | The effect of 3D surface mounted obstacles on laminar, incompressible marginally separated boundary layer flows |
scientific article; zbMATH DE number 1717583 |
Statements
7 March 2002
0 references
surface mounted obstacles
0 references
incompressible marginally separated boundary layer flows
0 references
viscous inviscid interaction
0 references
slender airfoil
0 references
laminar viscous wall jet
0 references
Goldstein singularity
0 references
marginal separation singularity
0 references
The effect of 3D surface mounted obstacles on laminar, incompressible marginally separated boundary layer flows (English)
0 references
Viscous inviscid interaction at incipient separation is considered in the following two cases: the boundary layer flow in the leading edge region of a slender airfoil at small angle of attack, and the flow of a laminar viscous wall jet on a flat plate impinging on a smoothed ramp. Above a critical value of the angle of attack/wall slope ratio, the calculation terminates in form of a Goldstein singularity. Finally, the authors also consider the marginal separation singularity.
0 references
