1–6 von 6 Ergebnissen
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    Investigations on Shock Control Bumps for Infinite Swept Wings

    Kutzbach, Martin / Lutz, Thorsten / Wagner, Siegfried | AIAA | 2004

    Numerical Optimization of Finite Shock Control Bumps

    Paetzold, Martin / Lutz, Thorsten / Kramer, Ewald et al. | AIAA | 2006

    Trailing-Edge Noise Measurements Using a Hot-Wire Based Coherent Particle Velocity Method

    Herrig, Andreas / Wuerz, Werner / Lutz, Thorsten et al. | AIAA | 2006

    Shock / Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings

    Ogawa, Hideaki / Babinsky, Holger / Pätzold, Martin et al. | AIAA | 2007

    An Implicit-Explicit Dirichlet-based Field Panel Method for Transonic Aircraft Design

    Gebhardt, Lutz / Fokin, Dmitri / Lutz, Thorsten et al. | AIAA | 2002

    Design and Wind-Tunnel Verification of Low-Noise Airfoils for Wind Turbines

    Lutz, Thorsten / Herrig, A / Wurz, W et al. | AIAA | 2006