Experimental evaluation of the effect of inlet distortion on compressor blade vibrations
- Lubomski, J. F.
- JAN 1, 1979.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Compressor rotor strain gage data from an engine test conducted with an inlet screen distortion were reduced and analyzed. These data are compared to data obtained from the same engine without inlet pressure distortion to determine the net effect of the distortion on the vibratory response of the compressor blades. The results obtained are presented.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19790008129.
Accession ID: 79N16300.
Intern. Gas Turbine Conf.; 12-15 Mar. 1979; San Diego, CA; United States.
- No Copyright.
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