Abstract
A procedure for the design of a strake mounted on a large forebody at a typical supersonic cruise condition is described. The design goal is attached flow on the upper surface of the strake at the low lift condition. Strake camber and thickness are systematically varied until an attached-flow, surface-pressure distribution is achieved. The surface pressures are computed by a full-potential solver, NHCOREL, and an empirical guideline is used to prevent leading-edge flow separation
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