NASA NTRS · 19810018560
Abradable compressor and turbine seals, volume 2
Abstract
The applications and advantages of abradable coatings as gas path seals in a general aviation turbofan engine were investigated. Abradable materials were evaluated for the high pressure radial compressor and the axial high and low pressure turbine shrouds.
Keep this discovery
Explore connections, maps & timelines
Sundberg, D. V., Dennis, R. E., Hurst, L. G.. 1979-07-01. Abradable compressor and turbine seals, volume 2. https://ntrs.nasa.gov/citations/19810018560
Cite the original work for its findings. Save a collection to share your selection of sources.