Funding for this research was provided by:
Aeronautical Science Foundation of China (2023Z037052002)
Article Title: Numerical investigation on discharge characteristics and aerodynamic effects of plasma synthetic jet actuator under low-pressure conditions
Journal Title: Physica Scripta
Article Type: paper
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Publication dates
Date Received: 2025-04-01
Date Accepted: 2025-07-08
Online publication date: 2025-07-23