1–16 von 16 Ergebnissen
|

    Numerical Simulation of Hovering S-76 Helicopter Rotor Including Far-Field Analysis (AIAA 2016-0034)

    Gardarein, Patrick / Le Pape, Arnaud | British Library Conference Proceedings | 2016

    CFD Investigations on a NACA0036 Airfoil with Active Flow Control

    Potsdam, Mark / Le Pape, Arnaud | AIAA | 2008

    Numerical Study of Flow Separation Control over a OA209 Airfoil Using Deployable Vortex Generator

    Joubert, Gilles / Le Pape, Arnaud / Huberson, Serge | AIAA | 2011

    Far-Field Analysis of Hovering Helicopter Rotor

    Le Pape, Arnaud / Verley, Simon / Destarac, Daniel | British Library Conference Proceedings | 2015

    Zonal Detached Eddy Simulation (ZDES) of an airfoil in post-stall condition

    Le Pape, Arnaud / Richez, François / Deck, S. | AIAA | 2012

    Zonal Detached-Eddy Simulation (ZDES) of the Three-dimensional Stalled Flow around a Finite Span Wing

    Richez, François / Le Pape, Arnaud / Costes, Michel et al. | AIAA | 2012

    Improved aerodynamic design of turbomachinery bladings by numerical optimization

    Burguburu, Stéphane / le Pape, Arnaud | Elsevier | 2002

    Wind Tunnel Assessment of the Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators

    Zanotti, Alex / Boniface, Jean-Christophe / Gaveriaux, Robert et al. | British Library Conference Proceedings | 2016

    Comparing Numerical and Experimental Results for Drag Reduction by Active Flow Control Applied to a Generic Rotorcraft Fuselage

    Allan, Brian G. / Le Pape, Arnaud / Schaeffler, Norman W. et al. | British Library Conference Proceedings | 2015

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

    Mulleners, Karen / Henning, Arne / Mai, H et al. | AIAA | 2009

    Investigation of unsteady flow development over a pitching airfoil by means of TR-PIV

    Freier Zugriff
    Mulleners, Karen / Henning, Arne / Mai, Holger et al. | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2009