Flow and Heat Transfer in Rotating Compressor Cavities With Inverted Shroud-Throughflow Temperature Differences (2025)
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1115/1.4067075
Publication URI: http://dx.doi.org/10.1115/1.4067075
Type: Journal Article/Review
Parent Publication: Journal of Turbomachinery
Issue: 7