NASA NTRS · 19850002691
Advanced blade tip seal system, volume 2
Abstract
The results of the endurance and performance engine tests conducted on monocrystal/abrasive-tipped CF6-50 Stage 1 HPT blades fabricated in Task VII of MATE Project 3 are presented. Two engine tests are conducted. The endurance engine test is conducted for 1000 C cycles. The performance engine test is conducted on a variable cycle core engine. Posttest evaluation and analyses of the blades and shrouds included visual, dimensional, and destructive evaluations.
Keep this discovery
Explore connections, maps & timelines
Zelahy, J. W., Fairbanks, N. P.. 1982-02-01. Advanced blade tip seal system, volume 2. https://ntrs.nasa.gov/citations/19850002691
Cite the original work for its findings. Save a collection to share your selection of sources.