Periodic Unsteady Tip Clearance Vortex Development in a Low-Speed Axial Research Compressor at Different Tip Clearances

Research output: Contribution to journalResearch articleContributedpeer-review

Contributors

Details

Original languageEnglish
Article number031005
Number of pages10
JournalJournal of Turbomachinery
Volume140
Issue number3
Publication statusPublished - 2018
Peer-reviewedYes

External IDs

Scopus 85039768153
ORCID /0000-0003-0900-8298/work/204616171

Keywords

Keywords

  • Verdichter Aerodynamik