Abstract This paper forms a fundamental part of the investigations on the theory of the aerodynamical lift, which have been devoloped by the author during the last years of the Pacific War. He takes the point of view of the acceleration potential propounded by L. Prandtl in 1936, as the starting point, which presents a special covenience to the treatment of the high speed problems and oscillating airfoils. We obtain, by application of Huygens' principle and the idea of Lorentz transformation concerning the classical wave equation, which governs the potential function of the field of small disturbances caused by the motion of the lifting system at high speed, the fundamental formulas of the acceleration and velocity field. The expression of the former obtained from Kirchhoff's formula concerning the field of pressure around the airfoil, linearly and automatically splits into two parts, one of which is the effect of the camber form of the wing section, while the other is the effect of the thickness. We also obtain the fundamental formula of the oscillaling lifting surface which is proved to be equivalenl to Kuu89ssner's.
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