Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity
Year: 2025
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4069800
Authors: Ruonan Wang, John W. Chew, Feng Gao, Olaf Marxen
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: China Scholarship Council
Award: G6329708033
OpenAlex ID: W7081952003
