Gezichtspunt van de reders m.b.t. Energiebesparing en stand van zaken en genomen maatregelen bij Nedlloyd

On the role of laminar separation bubbles in airfoil leading edge stalls

Design of a calculation method for 3D turbulent boundary layers

Boundary layer measurements on a two-dimensional wing with flap and a comparison with calculations

A method for the calculation of 3D boundary layers on practical wing configurations

Boudary layer measurements on a two-dimensional wing with flap

Tweede interimrapport over "Het inbouwen van viskeuze effecten in de panelenmethode voor profielen met kleppen"

European research programme on viscous flows : Eurovisc Annual Report

Samenvatting en enige konklusies

Calculation of the flow around a swept wing, taking into account the effect of the three-dimensional boundary layer. Part II: Wing with laminar boundary layer on the lower surface

Investigations of three-dimensional incompressible turbulent boundary layers

Radiation from a Point Charge Moving through a Circular Aperture in a Screen

Calculation of the flow around a swept wing, taking into account the effect of the three-dimensional boundary layer. Part I: Wing with turbulent boundary layer

Three-dimensional separation of an incompressible turbulent boundary layer on an infinite swept wing

A three-dimensional law of the wall for turbulent shear flows

Measurements in an incompressible three-dimensional turbulent boundary layer under infinite swept wing conditions and a comparison with theory

The law of the wall in two- and three- dimensional turbulent boundary layers

Measurements in a three-dimensional incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions

Voorstel voor een meetopstelling voor drie-dimensionaal grenslaagonderzoek in de LST 3x2

Voorstel voor een nieuwe lage-snelheid windtunnel voorzien van een meetplaats van 8x6 m. Deelrapport 2: Aerodynamische aspecten van het circuit