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Actions for Use of stage-stacking technique for predict- ing over-all performance in multistage axial- flow compressor utilizing interstage-air bleed
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Use of stage-stacking technique for predict- ing over-all performance in multistage axial- flow compressor utilizing interstage-air bleed
Author
Lucas, J. G.
Published
Oct 1, 1958.
Physical Description
1 electronic document
Online Version
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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Stage-stacking technique for predicting over-all performance in multistage axial flow turbojet compressor using interstage-air bleed
Other Subject(s)
AERODYNAMICS
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19650003121.
Accession ID: 65N12722.
NASA-MEMO-10-4-58E.
Terms of Use and Reproduction
No Copyright.
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| catkey: 15960102