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Inlet-air Distortion Effects on Stall, Surge, and Acceleration Margin of a Turbojet Engine Equipped with Variable Compressor Inlet Guide Vanes

Author
Harry, David P , III
Published
October 4, 1955.
Physical Description
1 electronic document
Additional Creators
Lubick, Robert J
Online Version

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: 19930088581.
Accession ID: 93R17871.
NACA-RM-E54K26.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15429943