Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant
Year: 2024
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4067237
Institution: Technische Universität Darmstadt
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G6931457741
OpenAlex ID: W4404595790