Experimental and numerical investigation of porous bleed control for supersonic/subsonic flows, and shock-wave/boundary-layer interactions-Reference-Cited by-同舟云学术

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Experimental and numerical investigation of porous bleed control for supersonic/subsonic flows, and shock-wave/boundary-layer interactions

Published:2024-04 Issue: Volume:147 Page:109062
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Giehler Julian^ORCID,Leudiere Thibault,Morgadinho Robert Soares,Grenson Pierre^ORCID,Bur Reynald^ORCID

Funder

European Commission

Horizon 2020

Horizon 2020 Marie Skłodowska-Curie Actions

Publisher

Elsevier BV

Reference43 articles.

1. Flow physics involved in shock wave/boundary layer interaction control;Délery,1999

2. Shock Wave–Boundary-Layer Interactions;Babinsky,2011

3. Pseudo-shock waves and their interactions in high-speed intakes;Gnani;Prog. Aerosp. Sci.,2016

4. Review of research into shock control bumps;Bruce;Shock Waves,2015

5. Investigation of three-dimensional shock control bumps for transonic buffet alleviation;D'Aguanno;AIAA J.,2023

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