1–20 von 38 Ergebnissen
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    Aerodynamic Shape Optimization of Hovering Rotors Using a Discrete Adjoint of the RANS Equations

    Dumont, A. / Le Pape, A. / Petert, J. et al. | British Library Conference Proceedings | 2009

    AIAA 2006-0687 Low Mach Number Preconditioning for Unsteady Flow in general "ALE" formulation

    Gleize, V. / Le Pape, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    AIAA 2006-1502 Improved Navier-Stokes Computations of a Stall-regulated Wind Turbine Using Low Mach number Preconditioning

    Le Pape, A. / Gleize, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    Automation ohne Unsicherheit: Vorstellung des Förderprojekts AutoAkzept zur Erhöhung der Akzeptanz automatisierten Fahrens

    Drewitz, U. / Ihme, K. / Oehl, M. et al. | British Library Conference Proceedings | 2019

    CFD Investigations on a NACA0036 Airfoil with Active Flow Control

    Potsdam, M. / Le Pape, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    CONCURRENT AERODYNAMIC OPTIMIZATION OF ROTOR BLADES USING A NASH GAME METHOD

    Leon, E.R. / Alfano, D. / Le Pape, A. et al. | British Library Conference Proceedings | 2013

    Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators

    Le Pape, A. / Costes, M. / Richez, F. et al. | AIAA | 2012

    Experimental investigations of rotor-fuselage aerodynamic interactions

    Pape, A. Le / Gatard, J. / Monnier, J.C. | Tema Archiv | 2007

    Experimental Study of Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators

    Costes, M. / David, F. / Deluc, J.-M. et al. | British Library Conference Proceedings | 2011

    Extensive Wind Tunnel Tests Measurements of Dynamic Stall Phenomenon for the OA209 Airfoil Including 3D Effects

    Le Pape, A. / Pailhas, G. / David, F. et al. | British Library Conference Proceedings | 2007

    Helicopter drag reduction by vortex generators

    Gibertini, G. / Boniface, J.C. / Zanotti, A. et al. | Elsevier | 2015

      Helicopter drag reduction by vortex generators

      Gibertini, G | Online Contents | 2015
      Beteiligte: Le Pape, A

    HELICOPTER FUSELAGE DRAG REDUCTION USING ACTIVE FLOW CONTROL: A COMPREHENSIVE EXPERIMENTAL INVESTIGATION

    Le Pape, A. / Pruvost, M. / Lienard, C. et al. | British Library Conference Proceedings | 2013

    Hovering Helicopter Rotor Experiments and Simulations in a Closed-Circuit Wind Tunnel

    Le Pape, A. / Massignon, M. / Crozier, P. et al. | British Library Conference Proceedings | 2007

    Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods

    Richter, K. / Knopp, T. / Garner, A.D. et al. | British Library Conference Proceedings | 2009

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

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

    Investigation of Dynamic Stall Control by Deployable Vortex Generator Using Time-Resolved PIV Analysis and URANS Computations

    Le Pape, A. / Heine, B. / Huberson, S. et al. | British Library Conference Proceedings | 2012

      Investigation of Dynamic Stall Control by Deployable Vortex Generator Using Time-Resolved PIV Analysis and URANS Computations

      Le Pape, A. / Heine, B. / Huberson, S. et al. | British Library Conference Proceedings | 2012

    Investigation of the Unsteady Flow Development Over a Pitching Airfoil by Means of TR-PIV

    Mulleners, K. / Henning, A. / Raffel, M. et al. | British Library Conference Proceedings | 2009