Experimental Study of Supersonic Film Cooling on Curved Wall at Mach 6
Year: 2025
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j065870
Authors: Zhen Zhang, Shihe Yi, Xiaolin Liu, Mengqi Zhang
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4414530453
