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    INFLUENCE OF OSCILLATION AMPLITUDE AND MACH NUMBER ON THE UNSTEADY TRANSITION ON A PITCHING ROTOR BLADE AIRFOIL

    Richter, K. / Koch, S. / Gardner, A.D. et al. | British Library Conference Proceedings | 2013

    EXPERIMENTAL INVESTIGATION OF AIR JETS TO CONTROL SHOCK-INDUCED DYNAMIC STALL

    Gardner, A.D. / Richter, K. / Mai, H. et al. | British Library Conference Proceedings | 2013

    Influence of Rotation on Dynamic Stall

    Gardner, A.D. / Richter, K. / Vertical Flight Technical Society | British Library Conference Proceedings | 2012

    Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows

    Richter, K. / Rosemann, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Improved two-dimensional dynamic stall prediction with structured and hybrid numerical methods

    Richter, K. / Pape, A. Le / Knopp, T. et al. | Tema Archiv | 2009

    NUMERICAL INVESTIGATION ON THE AERODYNAMIC EFFECT OF MINI-TEDS ON THE AWIATOR AIRCRAFT CONFIGURATION AT CRUISE CONDITIONS

    Richter, K. / Rosemann, H. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006

    Adaptive load redistribution using mini-TEDs

    Gardner, A.D. / Nitzsche, J. / Neumann, J. et al. | Tema Archiv | 2006

      ADAPTIVE LOAD REDISTRIBUTION USING MINI-TEDS

      Gardner, A. D. / Nitzsche, J. / Neumann, J. et al. | British Library Conference Proceedings | 2006