Film-Cooling Performance Comparison of Blade Tips With a Trailing Edge, Pressure Side Cutback, or a Suction Side Squealer in a Transonic Linear Cascade
Year: 2024
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4066911
Authors: Ming-Feng Yeh, Timothy A. Burdett, Lesley M. Wright, Je-Chin Han
Institutions: Texas A&M University, Messiah University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4403484513