Receptivity of a Transitional Shock/Boundary-Layer Interaction to Shock Oscillations in Hypersonic Flow
Year: 2026
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j066062
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Office of Naval Research
Award: G5249736366
OpenAlex ID: W7127041121
