1–20 of 34 hits
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    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

    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

    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

    Zonal Detached-Eddy Simulation of an Airfoil in Poststall Condition

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

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

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

    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

    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

    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

    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

    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

    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

    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

    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

    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

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

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

    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

    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

    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