Hoeijmakers, Hendrik Willem Marie (1948-)

A computational model for the calculation of the flow about wings with leading-edge vortices / by H. W. M. Hoeijmakers and B. Bennekersschema:ProductModel A higher-order panel method applied to vortex sheet roll-up / by H.W.M. Hoeijmakers and W. Vaatstraschema:ProductModel A higher-order panel method for the computation of the flow about slender delta wings with leading-edge vortex separation / by H.W.M. Hoeijmakers and W. Vaatstraschema:ProductModel A method for computing the three-dimensional flow about wings with leading-edge vortex separation / H.W.M. Hoeijmakersschema:ProductModel A method for computing the three-dimensional flow about wings with leading-edge vortex separation / H.W.M. Hoeijmakersschema:ProductModel A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow / by H.W.M. Hoeijmakersschema:ProductModel A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow / H.W.M. Hoeijmakersschema:ProductModel A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow / H.W.M. Hoeijmakersschema:ProductModel A panel method for the prediction of aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow / by H.W.M. Hoeijmakersschema:ProductModel Aërodynamica: wiskundige modellen in een stroomversnelling / H.W.M. Hoeijmakersschema:ProductModel An approximate method for computing inviscid vortex wake roll-up / by H.W.M. Hoeijmakersschema:ProductModel An approximate method for computing inviscid vortex wake roll-up / H.W.M. Hoeijmakersschema:ProductModel An approximate method for computing inviscid vortex wake roll-up / H.W.M. Hoeijmakersschema:ProductModel Application of an euler-equation method to a sharp-edged delta-wing configuration with vortex flow / by H.W.M. Hoeijmakers and J.I. van den Bergschema:ProductModel Aspects of second- and third-order panel methods demonstrated for the two-dimensional flat plate problem / H.W.M. Hoeijmakersschema:ProductModel Aspects of the modeling and numerical simulation of leading-edge vortex flow / by H.W.M. Hoeijmakersschema:ProductModel Computational aerodynamics of ordered vortex flows / by H.W.M. Hoeijmakersschema:ProductModel Computational aerodynamics of ordered vortex flows / Hendrik Willem Marie Hoeijmakersschema:ProductModel Computational vortex flow aerodynamics / by H.W.M. Hoeijmakersschema:ProductModel Methods for numerical simulation of leading-edge vortex flow / by H.W.M. Hoeijmakers H.W.M. Hoeijmakersschema:ProductModel ... show all 32

An experimental study of the flow over a sharp-edged delta wing at subsonic and transonic speeds / by A. Elsenaar and H.W.M. Hoeijmakersschema:ProductModel Analysis of results of an euler-equation method applied to leading-edge vortex flow / by J.I. van den Berg, H.W.M. Hoeijmakers and J.M.J.W. Jacobsschema:ProductModel Aspects of the application of an Euler-equation method to the simulation of leading-edge vortex flow / by J.M.J.W. Jacobs and H.W.M. Hoeijmakersschema: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 Numerical investigation into high-angle-of-attack leading-edge vortex flow / by J.I. van den Berg, H.W.M. Hoeijmakers, H.A. Sytsmaschema:ProductModel Numerical investigation into vortical flow about a delta-wing configuration up to incidences at which vortex breakdown occurs in experiment / by J.I. van den Berg, H.W.M. Hoeijmakers, F.J. Brandsmaschema:ProductModel Study into the limits of an Euler equation method applied to leading-edge vortex flow / by J.I. van den Berg, H.W.M. Hoeijmakers and H.A. Sytsmaschema:ProductModel