1. A. Le Pape, G. Pailhas, F. David, J.-M. Deluc, Extensive wind tunnel measurements of dynamic stall phenomenon for the OA209 airfoil including 3D effects, in: 33rd European Rotorcraft Forum, Kazan, Russia, September 2007.
2. M. Costes, V. Gleize, A. Le Pape, F. Richez, Numerical investigation of laminar/turbulent transition effects on the dynamic stall of an oscillating airfoil, in: American Helicopter Society Specialist Conference on Aeromechanics, San Francisco, CA, January 23–25, 2008.
3. Improved two-dimensional dynamic stall prediction with structured and hybrid numerical methods;Richter;J. Am. Helicopter Soc.,2011
4. Dynamic stall control using deployable leading-edge vortex generators;Le Pape;AIAA J.,2012
5. Vortical interactions behind deployable vortex generator for airfoil static stall control;Joubert;AIAA J.,2013