NASA NTRS · 19760017149
Single stage, low noise, advanced technology fan. Volume 2: Structural design
Abstract
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.
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Schoener, J. L., Black, G. R., Roth, R. H.. 1976-03-01. Single stage, low noise, advanced technology fan. Volume 2: Structural design. https://ntrs.nasa.gov/citations/19760017149
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