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Gas turbine rotor/case structural response to rotating stall: Experimental documentation and analytical approach

NASA NTRS · Conference Paper · 19830007383 · Published 2019-06-23 · Legacy CDMS · 1 author

Abstract and citation only, verbatim from NASA NTRS; full text lives there. All credit to the authors and Legacy CDMS.

Abstract

The forcing functions and structural responses characterizing gas turbine rotor/case system vibration due to rotating stall in an axial flow compressor are described. Two data sets with fundamentally different response characteristics are presented; one is supersynchronous and the other subsynchronous. Conventional beam element rotor dynamics analysis is shown to be severely limited in its ability to predict these responses. A new analytical approach, which significantly increases structural response predictive capability for these phenomena, is briefly discussed.

Author

  • Haley, P. J. Detroit Diesel Allison

Citation

Haley, P. J. (2019). Gas turbine rotor/case structural response to rotating stall: Experimental documentation and analytical approach. Legacy CDMS. NASA NTRS ID 19830007383. https://ntrs.nasa.gov/citations/19830007383 ↗