Three-Dimensional Flow over Wings with Leading-Edge Vortex Separation

This publication has 9 references indexed in Scilit:

• Boundary-Value Problem of Configurations with Compressible Free Vortex Flow
  AIAA Journal, 1977
• A numerical technique for subsonic flows past three dimensional canard-wing configurations with edge separations
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
• Three-Dimensional Solution of Flows over Wings with Leading-Edge Vortex Separation
  AIAA Journal, 1976
• A higher order panel method for general analysis and design applications in subsonic flow
  Published by Springer Nature ,1976
• Nonlinear Prediction of Aerodynamic Loads on Lifting Surfaces
  Journal of Aircraft, 1976
• Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex Configurations
  AIAA Journal, 1975
• Advanced panel-type influence coefficient methods applied to subsonic flows
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
  Journal of Aircraft, 1971
• A theory of the flow past a slender delta wing with leading edge separation
  Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959