@inproceedings{KleinStollbergMarkowskietal., author = {Klein, Robert and Stollberg, Christian and Markowski, Jens and Willscher, S. and Ay, Peter}, title = {Biodissolution for recovery of precious metals from electronic scrap}, series = {Proceedings of the XXIII International Mineral Processing Congress, Istanbul, Turkey 3-8 September 2006, Vol. 2}, booktitle = {Proceedings of the XXIII International Mineral Processing Congress, Istanbul, Turkey 3-8 September 2006, Vol. 2}, editor = {{\"O}nal, G{\"u}ven}, publisher = {Promed Advertising Agency}, address = {Istanbul}, isbn = {975-7946-29-X}, pages = {1557 -- 1560}, language = {en} } @misc{KleinKesslerSchmidt, author = {Klein, Marten and Kessler, Robert William and Schmidt, Heiko}, title = {On the influence of a wavy leading edge on the aerodynamic drag of a wing: A numerical parameter study}, series = {STAB Jahresbericht 2023}, volume = {21/2023}, journal = {STAB Jahresbericht 2023}, publisher = {Deutsche Str{\"o}mungsmechanische Arbeitsgemeinschaft (STAB)}, address = {G{\"o}ttingen, Germany}, pages = {110 -- 111}, language = {en} } @misc{KleinKesslerSchmidt, author = {Klein, Marten and Kessler, Robert William and Schmidt, Heiko}, title = {Numerical investigation of drag reduction effects on a track bicycle fork using wings with a wavy leading edge}, series = {Proceedings in Applied Mathematics and Mechanics}, volume = {24}, journal = {Proceedings in Applied Mathematics and Mechanics}, publisher = {Wiley}, issn = {1617-7061}, doi = {10.1002/pamm.202400178}, pages = {1 -- 14}, abstract = {Reynolds-averaged Navier-Stokes (RANS) and large-eddy simulations (LES) of the flow around wings with a wavy leading edge (WLE) are conducted in order to assess the capabilities of a passive flow control strategy for drag reduction. The intended application is indoor track cycling with controlled flow conditions. A section of a single fork rod is investigated in order to make the numerical simulations feasible. The present study reveals that net drag reduction is possible by a nonsinusoidal modification of the leading edge of the wing. However, the drag reduction effect remains limited to a few percent. While RANS and LES yield the same drag coefficient for a reference case, RANS underestimates the drag reduction effect for a longer wing and the WLE cases, but exhibits otherwise a qualitatively similar trend as the LES. With the aid of RANS, an optimal geometry is obtained defined by the wavelength-to-chord length ratio of and the amplitude-to-chord length ratio of . Corresponding LES results give an indication of the origin of drag reduction by a hampered vortex shedding. The generation of smaller and more streamwise oriented vortical flow structures at the trailing edge and behind the WLE wing is correlated with significantly reduced lift fluctuations and drag reduction.}, language = {en} }