NASA NTRS · 19880013871
Supersonic axial-flow fan flutter
Abstract
Lane's (1957) analytical formulation of the unsteady pressure distribution on an oscillating two-dimensional flat plate cascade in supersonic axial flow has been developed into a computer code. This unsteady aerodynamic code has shown good agreement with other published data. This code has also been incorporated into an existing aeroelastic code to analyze the NASA Lewis supersonic through-flow fan design.
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Ramsey, John K.. 1988-05-01. Supersonic axial-flow fan flutter. https://ntrs.nasa.gov/citations/19880013871
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