Skip to content Skip to footer

Research Portal of the TU Dresden

The Impact of Reduced Blade Count and Tip Clearance Variation on the Flow Field of Axial Compressor Blade Rows

Research output: Contribution to journal › Research article › Contributed › peer-review

Contributors

Robert Kaltofen - , Chair of Turbomachinery and Flight Propulsion (Author)
Martin Lange - , Chair of Turbomachinery and Flight Propulsion (Author)
Enrique Sielaff - , Rolls-Royce Germany Ltd. & Co. KG (Author)
Patrick Grothe - , Rolls-Royce Germany Ltd. & Co. KG (Author)
Bernd Becker - , Rolls-Royce Germany Ltd. & Co. KG (Author)
Ronald Mailach - , Chair of Turbomachinery and Flight Propulsion (Author)

Details

Original language	English
Article number	101008
Number of pages	10
Journal	Journal of turbomachinery
Volume	148
Issue number	10
Early online date	15 Sept 2026
Publication status	Published - Oct 2026
Peer-reviewed	Yes

External IDs

ORCID	/0000-0003-0900-8298/work/229892552

Keywords