A Theory of Supercritical Wing Sections, with Computer Programs and Examples

A Theory of Supercritical Wing Sections, with Computer Programs and Examples

With Computer Programs and Examples

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At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribut...