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- W2001877030 abstract "The subsonic/transonic stall flutter characteristics of the Pratt & Whitney PW1120 Low Pressure Compressor (LPC), recently have been defined through fan rig tests and a full-scale engine test. Flutter data analyses, based on both empirical and analytical methods, have shown excellent correlations between test results and predictions. While the LPC was demonstrated to be flutter-free over its entire flight envelope, the study indicates the need for continued research in transonic unsteady aerodynamics, particularly, the effects of passage shocks and large leading edge incidence." @default.
- W2001877030 created "2016-06-24" @default.
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- W2001877030 date "1986-06-08" @default.
- W2001877030 modified "2023-09-26" @default.
- W2001877030 title "Subsonic/Transonic Stall Flutter Investigation of an Advanced Low Pressure Compressor" @default.
- W2001877030 doi "https://doi.org/10.1115/86-gt-90" @default.
- W2001877030 hasPublicationYear "1986" @default.
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