Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge Separation

• 1 February 1974
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
• Vol. 11  (2) , 127-128
• https://doi.org/10.2514/3.60336

Abstract

Keywords

• DELTA WINGS
• VORTICES
• WING LOADING
• FINITE ELEMENT METHOD
• ANGLE OF ATTACK