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Single stage, low noise, advanced technology fan. Volume 2 : Structural design

Author
Roth, R. H.
Published
Mar 1, 1976.
Physical Description
1 electronic document
Additional Creators
Black, G. R. and Schoener, J. L.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The structural design for a half-scale fan vehicle, which would have application on an advanced transport aircraft, is described. The single stage advanced technology fan was designed to a pressure ratio of 1.8 at a tip speed of 503 m/sec (1,650 ft/sec). This mechanical design report describes the fan rotor design and the design of various structures of the vehicle; eg, stators, casings, splitters, seals, adapters, etc.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19760017149.
Accession ID: 76N24237.
R76AEG258-VOL-2.
NASA-CR-134802.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15735783