1–34 of 34 hits
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    Zonal Detached-Eddy Simulation of an Airfoil in Poststall Condition

    Le Pape, A. / Richez, F. / Deck, S. | AIAA | 2013

    Numerical analysis of hub and fuselage drag breakdown of a helicopter configuration

    Renaud, T. / Le Pape, A. / Péron, S. | Online Contents | 2013

    Numerical investigation of three-dimensional effects during dynamic stall

    Costes, M. / Richez, F. / Le Pape, A. et al. | Elsevier | 2015

      Numerical investigation of three-dimensional effects during dynamic stall

      Costes, M | Online Contents | 2015
      Contributors: Le Pape, A

    Zonal Detached-Eddy Simulation of Separated Flow Around a Finite-Span Wing

    Richez, F. / Le Pape, A. / Costes, M. | AIAA | 2015

      Zonal Detached-Eddy Simulation of Separated Flow Around a Finite-Span Wing

      Richez, F | Online Contents | 2015
      Contributors: Le Pape, A

    Numerical aerodynamic optimization of helicopter rotors: multiobjective optimization in hover and forward flight conditions

    Le Pape, A. / Royal Aeronautical Society | British Library Conference Proceedings | 2005

    Vortical Interactions Behind Deployable Vortex Generator for Airfoil Static Stall Control

    Joubert, G. / Le Pape, A. / Heine, B. et al. | AIAA | 2012

      Vortical Interactions Behind Deployable Vortex Generator for Airfoil Static Stall Control

      Joubert, G | Online Contents | 2013
      Contributors: Le Pape, A

    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

    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

    Numerical and Experimental Investigation of Helicopter Fuselage Drag Reduction Using Active Flow Control

    Lienard, C. / Le Pape, A. / Verbeke, C. et al. | British Library Conference Proceedings | 2012

    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
      Contributors: Le Pape, A

    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

    THE GROUP OF RESPONSABLES ``ROTORCRAFT (RC-GOR)'': AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES

    Visingardi, A. / Heger, R. / Le Pape, A. et al. | British Library Conference Proceedings | 2022

    Numerical Investigation of Laminar/Turbulent Transition Effects on the Dynamic Stall of an Oscillating Airfoil

    Costes, M. / Gleize, V. / Le Pape, A. et al. | British Library Conference Proceedings | 2008

    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

    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

    ZONAL DETACHED EDDY SIMULATION (ZDES) OF AN AIRFOIL IN POST-STALL CONDITION

    Le Pape, A. / Richez, F. / Deck, S. et al. | British Library Conference Proceedings | 2012

    NUMERICAL STUDY OF FLOW SEPARATION CONTROL OVER A OA209 AIRFOIL USING DEPLOYABLE VORTEX GENERATOR

    Joubert, G. / Le Pape, A. / Huberson, S. et al. | British Library Conference Proceedings | 2011

    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

    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

    Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators

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

    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

    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

    ZONAL DETACHED-EDDY SIMULATION (ZDES) OF THE THREE-DIMENSIONAL STALLED FLOW AROUND A FINITE SPAN WING

    Richez, F. / Costes, M. / Le Pape, A. et al. | British Library Conference Proceedings | 2012

    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

    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

    Numerical Simulation of a Pitching Airfoil Under Dynamic Stall Conditions Including Laminar/Turbulent Transition

    Gleize, V. / Costes, M. / Le Pape, A. et al. | British Library Conference Proceedings | 2008

    Sensitivity Analysis Using Direct Differentiation and ADjoint Vector Methods for Helicopter Rotor Flow In Hover

    Dumont, A. / Le Pape, A. / Peter, J. et al. | British Library Conference Proceedings | 2008

    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

    Wind-Tunnel Assessment of the Concept of Active Flaps on a Helicopter Rotor Model

    Delrieux, Y. / Le Pape, A. / Leconte, P. et al. | British Library Conference Proceedings | 2007

    Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction

    Zanotti, A | Online Contents | 2016
    Contributors: Le Pape, A