NASA NTRS · 19770010116
Reverse pitch fan with divided splitter
Abstract
A guide vane arrangement is described for improving gas turbine performance in the reverse thrust mode. This flow straightening method produces low losses in the fluid entering a core engine during reverse thrust operations and allows large supercharging of the core engine during forward thrust.
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Smith, L. H., Jr.. 1977-02-01. Reverse pitch fan with divided splitter. https://ntrs.nasa.gov/citations/19770010116
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