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Application of TURBO-AE to Flutter Prediction: Aeroelastic Code DevelopmentThe 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 .
Document ID
20010047229
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Hoyniak, Daniel
(Rolls-Royce Allison Indianapolis, IN United States)
Simons, Todd A.
(Rolls-Royce Allison Indianapolis, IN United States)
Stefko, George
Date Acquired
September 7, 2013
Publication Date
May 1, 2001
Subject Category
Aerodynamics
Report/Patent Number
NASA/CR-2001-210761
EDR-19540
NAS 1.26:210761
Report Number: NASA/CR-2001-210761
Report Number: EDR-19540
Report Number: NAS 1.26:210761
Funding Number(s)
PROJECT: RTOP 708-28-13
CONTRACT_GRANT: NAS3-27725
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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