Work

Response of a tip gap flow submitted to an unsteady shock wave front

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0305018

Authors: C. Wingel, N. Binder, J. Gressier

Institutions: Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO), Université de Toulouse

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: Grand Équipement National De Calcul Intensif, Agence de l'innovation de Défense

Awards: G2248888547, G2463213048

OpenAlex ID: W4416994913

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Cites: 39

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