Effect of Ingress on Flow and Heat Transfer Upstream and Downstream of a Rotating Turbine Disc (2019)
Attributed to:
Experimental and theoretical modelling of hot-gas ingestion through gas-turbine rim seals
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.3390/aerospace6050049
Publication URI: http://dx.doi.org/10.3390/aerospace6050049
Type: Journal Article/Review
Parent Publication: Aerospace
Issue: 5