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Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine II-Analysis of Compressor Performance

Author:
Howard, Ephraim M.
Published:
August 23, 1948.
Physical Description:
1 electronic document
Additional Creators:
Dietz, Robert O., Jr. and Berdysz, Joseph J.
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary:
Compressor performance properties for two 11-stage compressors of 3000-pound-thrust axial-flow turbojet engines were determined. Data are presented for a range of simulated altitudes and a range of Mach numbers for various modifications of the engine.
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 20030064244.
NACA-RM-E8A26a.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15636639