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Actions for Turbine-rotor-blade Designs Based on One-dimensional-flow Theory I : Performance of Single-stage Turbine Having 40-percent Reaction
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Turbine-rotor-blade Designs Based on One-dimensional-flow Theory I : Performance of Single-stage Turbine Having 40-percent Reaction
Author
Hauser, Cavour H
Published
June 10, 1949.
Physical Description
1 electronic document
Additional Creators
English, Robert E
Online Version
hdl.handle.net
, Connect to this object online.
Full Text available online
Availability
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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930085897.
Accession ID: 93R15187.
NACA-RM-E9C15.
Terms of Use and Reproduction
No Copyright.
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| catkey: 15432075