NASA NTRS · 19920000109
Simulation Of Unsteady, Inviscid, Rotational, Transonic Flow
Abstract
Report describes numerical simulation of two-dimensional, unsteady, inviscid rotational, transonic flow about rigid airfoil in such motions as pitching or plunging oscillations. Study demonstrates potential utility of computation in analyses of aeroelasticity of airfoils.
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Damodaran, Murali. 1992-02-01. Simulation Of Unsteady, Inviscid, Rotational, Transonic Flow. https://ntrs.nasa.gov/citations/19920000109
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