Numerical modelling of shock wave-boundary layer interaction control by passive wall ventilation-Reference-Cited by-同舟云学术

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Numerical modelling of shock wave-boundary layer interaction control by passive wall ventilation

Published:2020-03 Issue: Volume:200 Page:104435
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Szulc O.^ORCID,Doerffer P.,Flaszynski P.,Suresh T.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference34 articles.

1. SBLI control for wings and inlets;Babinsky;Shock Waves,2008

2. EUROSHOCK: drag reduction by passive shock control;Stanewsky,1997

3. Drag reduction by shock and boundary layer control;Stanewsky,2002

4. Modelling of perforated plate aerodynamics performance;Doerffer;Aerosp Sci Technol,2000

5. Study of control devices applied to a transonic shock wave/boundary layer interaction;Bur,2002

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1. Numerical Study on Far-Field Noise Characteristic Generated by Wall-Mounted Swept Finite-Span Airfoil within Transonic Flow;Aerospace;2024-08-08

2. Effects of Perforated Plates on Shock Structure Alteration for NACA0012 Airfoils;Inventions;2024-03-05

3. Moving wall effect on normal shock wave–turbulent boundary layer interaction on an airfoil;International Journal of Numerical Methods for Heat & Fluid Flow;2023-12-20

4. Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade;Journal of Thermal Science;2023-12-06

5. Effects of Perforated Plates on the Performance of Vaned Diffusers for Microgas Turbines;2023 11th International Conference on ENERGY and ENVIRONMENT (CIEM);2023-10-26

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