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Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler o...

Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler o...

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_8fa4863cec84414ebd11f9f75718ad36

Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler of the Cavity in the Low-Aspect-Ratio Aircraft

About this item

Full title

Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler of the Cavity in the Low-Aspect-Ratio Aircraft

Publisher

Basel: MDPI AG

Journal title

Aerospace, 2022-09, Vol.9 (9), p.526

Language

English

Formats

Publication information

Publisher

Basel: MDPI AG

More information

Scope and Contents

Contents

The internal weapon bay is widely used in modern aircraft; however, because the unsteady flows of the cavity would cause dangerous store separation and intense aerodynamic noise, the leading-edge spoiler is an easy and efficient passive flow-control method. The flow control of the leading-edge flat spoiler before the cavity of a low-aspect-ratio fl...

Alternative Titles

Full title

Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler of the Cavity in the Low-Aspect-Ratio Aircraft

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_8fa4863cec84414ebd11f9f75718ad36

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_8fa4863cec84414ebd11f9f75718ad36

Other Identifiers

ISSN

2226-4310

E-ISSN

2226-4310

DOI

10.3390/aerospace9090526

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