A new, quasi-simultaneous method to calculate interacting boundary layers

A new, quasi-simultaneous method to calculate interacting boundary layers

Veldman, A.E.P.

National Aerospace Laboratory NLR

1980-02-29

A quasi-simultaneous method is described to calculate laminar, incompressible boundary layers interacting with an inviscid outer flow. The essential feature of this method is an interactive boundary condition prescribing a linear combination of pressure and displacement thickness which models the behaviour of the outer flow. This way the quasi-simultaneous method avoids difficulties incurred when either direct or inverse methods are used, resulting in fast convergence of the iterative procedure involved. The method is consistent with asymptotic triple-deck theory. Results will be presented for two problems which exhibit strong interaction between the viscous and inviscid regions: i) a boundary layer with a separation bubble, and ii) the flow near the trailing edge of a flat plate.

http://resolver.tudelft.nl/uuid:3e9bd34b-93ff-41f5-8fa1-6898f5f109f1

Nationaal Lucht- en Ruimtevaartlaboratorium

Campus only

NLR MP 80012 U

Aerospace Engineering Reports

report

(c) 1980 National Aerospace Laboratory NLR