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- Unclassified, Unlimited, Publicly available.
- The compressor case of a 13-stage axial-flow compressor was modified to incorporate air-bleed systems over the fifth and tenth rotor stages. Rotating stall-exited rotor-blade vibrations were measured in the first and second stages at 60 and 68 percent of rated speed, respectively. Either the fifth- or the tenth-stage bleeds satisfactorily eliminated the peak vibratory stresses.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19930089494.
Accession ID: 93R18784.
- No Copyright.
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