NASA NTRS · 19920004625
A numerical method for unsteady aerodynamics via acoustics
Abstract
Formal solutions to the wave equation may be conveniently described within the framework of generalized function theory. A generalized function theory is used to yield a formulation and formal solution of a wave equation describing oscillation of a flat plate from which a numerical method may be derived.
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Hodge, Steve. 1991-09-01. A numerical method for unsteady aerodynamics via acoustics. https://ntrs.nasa.gov/citations/19920004625
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