NASA NTRS · 20020034911
Aeroelastic Analysis for Aeropropulsion Applications
Abstract
Aeroelastic codes with advanced capabilities for modeling flow require substantial computational time. On the other hand, fast-running linear aeroelastic codes lack the capability to model three-dimensional, transonic, vortical, and viscous flows. The goal of this work was to develop an aeroelastic code with accurate modeling capabilities and small computational requirements.
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Keith, Theo G., Jr., Bakhle, Milind A.. 2002-01-01. Aeroelastic Analysis for Aeropropulsion Applications. https://ntrs.nasa.gov/citations/20020034911
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