Aerodynamic Design of High End Wall Angle Turbine Stages-Part I: Methodology Development (2014)
Attributed to:
SAMULET Project 1 - High Efficiency Turbomachinery
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1115/1.4023905
Publication URI: http://dx.doi.org/10.1115/1.4023905
Type: Journal Article/Review
Parent Publication: Journal of Turbomachinery
Issue: 2