Extension to the Panel Code NALSOP0509 to Include Designudof Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment

摘要

The code NALSOP0509, available in the SOFFTS Library of NALudhas been extended to include a design of wing-body combinations to, minimize induced drag for specified lift and pitching moments at sub- or super--sonic flow conditions, Method of Lagrangean multiple is used to obtain the optimum camber and twist distributions for the wing in the presence of a body. SOFFTS Library of NAL has now been updated with this version of the code.