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A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

E. D. Albano, William P. Rodden

Open publisher page 983 citations

Abstract

Approximate solutions from the linearized formulation are obtained by idealizing the surface as a set of lifting elements which are short line segments of acceleration-potential doub? lets. The normal velocity induced by an element of unit strength is given by an integral of the subsonic kernel function. The load on each element is determined, by, satisfying normal velocity boundary conditions at a set of points oil the surface. It is seen a posteriori

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What this paper is about

Approximate solutions from the linearized formulation are obtained by idealizing the surface as a set of lifting elements which are short line segments of acceleration-potential doub? lets. The normal velocity induced by an element of unit strength is given by an integral of the subsonic kernel function. The load on each element is determined, by, satisfying normal velocity boundary conditions at a set of points oil the surface. It is seen a posteriori

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Available abstract

Approximate solutions from the linearized formulation are obtained by idealizing the surface as a set of lifting elements which are short line segments of acceleration-potential doub? lets. The normal velocity induced by an element of unit strength is given by an integral of the subsonic kernel function. The load on each element is determined, by, satisfying normal velocity boundary conditions at a set of points oil the surface. It is seen a posteriori

Key concepts: Lift (data mining), Mechanics, Physics, Lift coefficient, Aerospace engineering, Classical mechanics, Geometry, Mathematics

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A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. — Research Paper | ScholarLens