Mechanical Engineering Faculty Research
Title
Flutter Stability of a Detuned Cascade in Subsonic Compressible Flow
Document Type
Article
Publication Date
Fall 9-1995
Abstract
A mathematical model is developed to predict the unsteady aerodynamics of a detuned two-dimensional flat plate cascade in subsonic compressible flow. Aerodynamic detuning is introduced by nonuniform circumferential spacing and chordwise offset. Combined aerodynamic-structural detuning is accomplished by replacing alternative airfoils with splitter blades...
Publication Title
Journal of Propulsion and Power
Volume
11
Issue
5
First Page
923
Last Page
930
Recommended Citation
Sawyer, Scott and Fleeter, Sanford, "Flutter Stability of a Detuned Cascade in Subsonic Compressible Flow" (1995). Mechanical Engineering Faculty Research. 857.
https://ideaexchange.uakron.edu/mechanical_ideas/857
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