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Windtunnel investigation with a two-dimensional airfoil on the effect of blowing over a flap and over a control surface
Windtunnel investigation with a two-dimensional airfoil on the effect of blowing over a flap and over a control surface
Windtunnel investigation on the effect of blowing over the flap and over the wing nose at various aspect ratios sweep angles and flap spans
Windtunnel investigation on the effect of blowing over the flap and over the wing nose at various aspect ratios sweep angles and flap spans
Enige beschouwingen over de kwaliteit van de stroming op de meetplaats van de LST 8x6 : Deel II : enige begrippen uit de statistische turbulentietheorie en de toepassing ervan op de berekening van de uitdemping en van de werking van gazen en van contracti
Enige beschouwingen over de kwaliteit van de stroming op de meetplaats van de LST 8x6 : Deel II : enige begrippen uit de statistische turbulentietheorie en de toepassing ervan op de berekening van de uitdemping en van de werking van gazen en van contractie
Reynolds number and Mach number effects on the maximum lift and the stalling characteristics of wings at low speeds
Reynolds number and Mach number effects on the maximum lift and the stalling characteristics of wings at low speeds
Some notes on two-dimensional high-lift tests in wind tunnels
Some notes on two-dimensional high-lift tests in wind tunnels
Voorstel voor een nieuwe lage-snelheid windtunnel voorzien van een meetplaats van 8x6 m. Deelrapport 2: Aerodynamische aspecten van het circuit
Voorstel voor een nieuwe lage-snelheid windtunnel voorzien van een meetplaats van 8x6 m. Deelrapport 2: Aerodynamische aspecten van het circuit
Voorstel voor een meetopstelling voor drie-dimensionaal grenslaagonderzoek in de LST 3x2
Voorstel voor een meetopstelling voor drie-dimensionaal grenslaagonderzoek in de LST 3x2
Measurements in a three-dimensional incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions
Measurements in a three-dimensional incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions
The law of the wall in two- and three- dimensional turbulent boundary layers
The law of the wall in two- and three- dimensional turbulent boundary layers
Measurements in an incompressible three-dimensional turbulent boundary layer under infinite swept wing conditions and a comparison with theory
Measurements in an incompressible three-dimensional turbulent boundary layer under infinite swept wing conditions and a comparison with theory
A three-dimensional law of the wall for turbulent shear flows
A three-dimensional law of the wall for turbulent shear flows
Three-dimensional separation of an incompressible turbulent boundary layer on an infinite swept wing
Three-dimensional separation of an incompressible turbulent boundary layer on an infinite swept wing
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
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
Radiation from a Point Charge Moving through a Circular Aperture in a Screen
Radiation from a Point Charge Moving through a Circular Aperture in a Screen
Investigations of three-dimensional incompressible turbulent boundary layers
Investigations of three-dimensional incompressible turbulent boundary layers
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
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
Samenvatting en enige konklusies
Samenvatting en enige konklusies
European research programme on viscous flows : Eurovisc Annual Report
European research programme on viscous flows : Eurovisc Annual Report
Tweede interimrapport over
Tweede interimrapport over "Het inbouwen van viskeuze effecten in de panelenmethode voor profielen met kleppen"
Boudary layer measurements on a two-dimensional wing with flap
Boudary layer measurements on a two-dimensional wing with flap
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