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 ↗