NASA NTRS · 19720021143
Highly loaded multi-stage fan drive turbine: Leaned stator configuration design
Abstract
The results of the high lift blade configuration design study are reported. The three-stage constant-inside-diameter turbine utilizes a ten degree tangentially leaned stator in stage three. All other bladerows use plain blades. Analysis of the leaned stator is discussed, and detailed design data are summarized. Steady-state stresses are discussed, and the results of the mechanical design analysis are presented.
Keep this discovery
Explore connections, maps & timelines
Evans, D. C., Wolfmeyer, G. W.. 1972-07-01. Highly loaded multi-stage fan drive turbine: Leaned stator configuration design. https://ntrs.nasa.gov/citations/19720021143
Cite the original work for its findings. Save a collection to share your selection of sources.