Numerical Investigation on Conjugate Heat Transfer in a Turbine Vane With Matrix Cooling Channel
Year: 2026
Type: article
DOI: 10.1115/1.4071832
Institution: Harbin Institute of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G1772229115
OpenAlex ID: W7160311658
