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The aerodynamic design of a compressor-drive turbine for use in a 75 kw automotive engine

Author
Mclallin, K. L.
Published
Apr 1, 1975.
Physical Description
1 electronic document
Additional Creators
Roelke, R. J.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The design specifications are given, and the aerodynamic design procedure is described. The aerodynamic information includes the results of flow path, velocity diagram, and blade profile studies. Predicted off-design performance characteristics are also presented.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19750013561.
Accession ID: 75N21633.
NASA-TM-X-71717.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15740355