Bruin, Anton C. de

Boundary-layer calculations on the leeward surface of a slender delta wing at incidence / by A.C. de Bruinschema:ProductModel Computation of three-dimensional boundary layer transition and separationon a 65 deg swept delta wing at 20 deg angle of attack / by A.C. de Bruin and H.W.M. Hoeijmakersschema:ProductModel Experiments and theoretical considerations regarding the allowable roughness height in laminar flow / by A.C. de Bruinschema:ProductModel Laminar and turbulent boundary-layer calculations on the leeward of a slender delta wing at incidence / by A.C. de Bruinschema:ProductModel New attempts to solve an old problem : aerodynamic measurements in new vehicle tunnels / by A.C. de Bruin, R.A. Maarsingh and L. Swartschema:ProductModel Turbulence modelling of the shear layers in the trailing edge region of a modern rear-loaded airfoil at incidence / by A.C. de Bruin, L.H.J. Absil and D.M. Passchierschema:ProductModel

A method for three-dimensional boundary layer calculations on arbitrary bodies; some results on aircraft wings and engine cowls / by J.P.F. Lindhout, A.C. de Bruin and J.H.M. Goodenschema:ProductModel Experimental pressure wave research at NLR for high-speed rail tunnels / E.A. Demmenie, A.C. de Bruin, E. Klaverschema:ProductModel Flow field survey in trailing vortex system behind a civil aircraft model at high lift / by A.C. de Bruin ... [et al.]schema:ProductModel