Unsteady shock wave behaviors in supersonic nozzle exit under varying over-expanded conditions
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0283192
Authors: Yi Yang, Qiancheng Wang, Yuxin Zhao, Gang He, Yilong Zhao
Institution: National University of Defense Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4413339433