Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows-Reference-Cited by-同舟云学术

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Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows

Published:2024-04 Issue: Volume:147 Page:109033
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sebastian Robin^ORCID,Schreyer Anne-Marie^ORCID

Funder

Center for High Performance Computing

Gauss Centre for Supercomputing

Deutsche Forschungsgemeinschaft

Publisher

Elsevier BV

Reference43 articles.

1. The application of boundary layer suction to suppress strong shock-induced separation in supersonic inlets;Wong,1974

2. Introduction to shock-induced separation and its prevention by design and boundary layer control;Pearcey,1961

3. The use of air jets for boundary layer control;Wallis,1952

4. Theoretical analysis of effects of boundary layer bleed on scramjet thrust;Yue;Sci. China, Phys. Mech. Astron.,2013

5. Review of research on low-profile vortex generators to control boundary-layer separation;Lin;Prog. Aerosp. Sci.,2002

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