Experimental and numerical study on double wedge shock/shock interaction controlled by a single-pulse plasma synthetic jet
Year: 2024
Type: article
Source: Plasma Science and Technology
Institution: National University of Defense Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G3294839953, G4019489240
OpenAlex ID: W4404315126