Induced Aerodynamics of Helicopters: Part I

Abstract

THE simple actuator disk theory, first postulated by Froude over sixty years ago, is the basis of most helicopter induced flow theory. This disk is an idealization of a rotor which uniformly accelerates the air with no loss of thrust at the blade tips. It can therefore be regarded as the limit case of a rotor with an infinite number of blades. It is also assumed to be infinitely thin so that no discontinuities in velocity occur on the two sides of the disk.

Citation

Payne, P.R. (1956), "Induced Aerodynamics of Helicopters: Part I", Aircraft Engineering and Aerospace Technology, Vol. 28 No. 2, pp. 46-51. https://doi.org/10.1108/eb032660