Aerodynamic Design of High Endwall Angle Turbine Stages: Part 1-Methodology Development (2012)
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/gt2012-68705
Publication URI: http://dx.doi.org/10.1115/gt2012-68705
Type: Conference/Paper/Proceeding/Abstract