1–20 von 37 Ergebnissen
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    A Numerical Study on the Ability of Shock Control Bumps for Buffet Alleviation

    Mayer, Rouven / Lutz, Thorsten / Kraemer, Ewald | AIAA | 2017

    UAV Icing: Numerical Simulation of Propeller Ice Accretion

    Müller, Nicolas / Hann, Richard / Lutz, Thorsten | AIAA | 2021

    Active Gust Alleviation on a High Aspect Ratio Wing Based on High Fidelity CFD Simulations

    Hillebrand, Marco / Müller, Jens / Lutz, Thorsten | AIAA | 2023

    Wind Tunnel Support System Influence on NASA Common Research Model at Low-Speed Conditions

    Waldmann, Andreas / Lutz, Thorsten / Krämer, Ewald | AIAA | 2018

    Wind Tunnel Support System Influence on NASA Common Research Model at Low Speed Conditions

    Waldmann, Andreas / Lutz, Thorsten / Kraemer, Ewald | AIAA | 2016

    Vortical structures on three-dimensional shock control bumps

    Colliss, Simon / Babinsky, Holger / Nubler, Klemens et al. | AIAA | 2013

    Transonic Tail Buffet Simulations for the Common Research Model

    Illi, Sebastian / Fingskes, Christian / Lutz, Thorsten et al. | AIAA | 2013

    CFD-based Studies of Propeller Sizing and Operation Settings for High-Lift Applications of Distributed Propulsion

    Firnhaber Beckers, Mário / Kern, Maximilian / Schollenberger, Michael et al. | AIAA | 2023

    Numerical Optimization of Finite Shock Control Bumps

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

    Rnoise: A RANS Based Airfoil Trailing-edge Noise Prediction Model

    Kamruzzaman, Mohammad / Bekiropoulos, Dimitrios / Wolf, Alexander et al. | AIAA | 2014

    Passive Control of the Flow Around the Stratospheric Observatory for Infrared Astronomy

    Schmid, Sven / Lutz, Thorsten / Krämer, Ewald et al. | AIAA | 2008

    Shock Control Bump Robustness Enhancement

    Nuebler, Klemens / Lutz, Thorsten / Kraemer, Ewald et al. | AIAA | 2012

    Unsteady Wake of the NASA Common Research Model in Low-Speed Stall

    Waldmann, Andreas / Gansel, Philipp P. / Lutz, Thorsten et al. | AIAA | 2015

    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 experimental investigation of three-dimensional shock control bumps applied to transonic airfoils

    Colliss, Simon / Babinsky, Holger / Bruce, Paul et al. | AIAA | 2012