📣 Help Shape the Future of UKRI's Gateway to Research (GtR)

We're improving UKRI's Gateway to Research and are seeking your input! If you would be interested in being interviewed about the improvements we're making and to have your say about how we can make GtR more user-friendly, impactful, and effective for the Research and Innovation community, please email gateway@ukri.org.

Effect of Ingress on Flow and Heat Transfer Upstream and Downstream of a Rotating Turbine Disc (2019)

First Author: Tang H

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