NASA NTRS · 20010047229
Application of TURBO-AE to Flutter Prediction: Aeroelastic Code Development
Abstract
The TURBO-AE program has been evaluated by comparing the obtained results to cascade rig data and to prediction made from various in-house programs. A high-speed fan cascade, a turbine cascade, a turbine cascade and a fan geometry that shower flutter in torsion mode were analyzed. The steady predictions for the high-speed fan cascade showed the TURBO-AE predictions to match in-house codes. However, the predictions did not match the measured blade surface data. Other researchers also reported similar disagreement with these data set. Unsteady runs for the fan configuration were not successful using TURBO-AE .
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Hoyniak, Daniel, Simons, Todd A., Stefko, George. 2001-05-01. Application of TURBO-AE to Flutter Prediction: Aeroelastic Code Development. https://ntrs.nasa.gov/citations/20010047229
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