Research on supersonic film cooling of hypersonic optical window under different nozzle pressure ratios
Year: 2024
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0230116
Institution: National University of Defense Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G1269711760, G4386357015, G4938697759
OpenAlex ID: W4403401660
