Heat transfer performance optimization of turbine blade internal cooling channel with pin-fins and recessed-extruded endwalls
Year: 2024
Type: article
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Trường Đại học Bách Khoa Hà Nội
Award: G2116659928
OpenAlex ID: W4403225718
