Aerodynamic Feasibility Investigation of the Novel Experimental Rig on Turbine Blade Tip With High Relative Motion
Year: 2024
Type: article
DOI: 10.1115/1.4066534
Institution: Shanghai Jiao Tong University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4402514685
