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Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor

Author
Cullom, R. R.
Published
Oct 1, 1959.
Physical Description
1 electronic document
Additional Creators
Goldstein, A. W. and Schacht, R. L.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Overall stage and stator blade element performance with straight stator and tilted stator in transonic axial flow compressor stage
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19650003088.
Accession ID: 65N12689.
NASA-TM-X-99.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15960132