Through the empirical correlation of experimental data and theoretical analysis, a set of graphs has been developed which summarize the inviscid aerodynamics of delta wings at supersonic speeds. The various graphs which detail the aerodynamic performance of delta wings at both zero-lift and lifting conditions were then employed to define a preliminary wing design approach in which both the low-lift and high-lift design criteria were combined to define a feasible design space. Wood, Richard M. Langley Research Center AERODYNAMICS; DELTA WINGS; INVISCID FLOW; SUPERSONIC AIRFOILS; SUPERSONIC SPEED; AERODYNAMIC LOADS; DESIGN ANALYSIS; EXPERIMENT DESIGN; FRICTION DRAG; LIFT; NONLINEAR SYSTEMS; WINGS...