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Llorente, Elena (author), Ragni, D. (author)
A study of the aerodynamic performance of a NACA 643418 airfoil with trailing edge serrations is presented. For the prediction of the changes in lift due to the serration installation, an empirical law is derived that can be extended to typical cambered airfoils for wind turbine applications. The law is deduced from 2D and 3D Reynolds‐averaged...
journal article 2019
document
Jin, W. (author), Kleijn, C.R. (author), van Ommen, J.R. (author)
For simulating rarefied gas flows around a moving body, an immersed boundary method is presented here in conjunction with the Direct Simulation Monte Carlo (DSMC) method in order to allow the movement of a three dimensional immersed body on top of a fixed background grid. The simulated DSMC particles are reflected exactly at the landing...
conference paper 2016
document
Terra, W. (author), Sciacchitano, A. (author), Scarano, F. (author)
Aerodynamic drag is computed from velocity measurements obtained with particle image velocimetry (PIV). This allows determining the drag force in combination with the visualization of the flow structures responsible for drag generation. Two experiments are conducted to illustrate the working principle of the approach, which is meant for...
journal article 2016
document
Breugem, W.P. (author), Boersma, B.J. (author)
A direct numerical simulation (DNS) has been performed of turbulent channel flow over a three-dimensional Cartesian grid of 30×20×9 cubes in, respectively, the streamwise, spanwise, and wall-normal direction. The grid of cubes mimics a permeable wall with a porosity of 0.875. The flow field is resolved with 600×400×400 mesh points. To enforce...
journal article 2005
document
Boogaard, H.F.P. van den (author), Uittenbogaard, R.E. (author), Gerritsen, H. (author)
report 1991
document
Deelen, C. (author)
report 1980
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