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With the aid of that solutions of airfoil and using supersonic linearized theory, the closed approximate expression of unsteady loading distribution is givers for rectangular wings in pitching and plunging oscillations. ...Thus, the computation method of this paper extends the application scope of Hui's(Refs.1,2) theory that hoMs for low frequency(k∞ ⪡1) pitching oscillation, Comparisons with supersonic linearized, Van Dyke and Lighthill theories are given.