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A decomposition formula for the wall heat flux of a compressible boundary layer

A decomposition formula for the wall heat flux of a compressible boundary layer

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_80f7f5b80b324dffb455befad500b18a

A decomposition formula for the wall heat flux of a compressible boundary layer

About this item

Full title

A decomposition formula for the wall heat flux of a compressible boundary layer

Publisher

Singapore: Springer Singapore

Journal title

Advances in aerodynamics, 2021-11, Vol.3 (1), p.1-13, Article 33

Language

English

Formats

Publication information

Publisher

Singapore: Springer Singapore

More information

Scope and Contents

Contents

Understanding the generation mechanism of the heat flux is essential for the design of hypersonic vehicles. We proposed a novel formula to decompose the heat flux coefficient into the contributions of different terms by integrating the conservative equation of the total energy. The reliability of the formula is well demonstrated by the direct numer...

Alternative Titles

Full title

A decomposition formula for the wall heat flux of a compressible boundary layer

Authors, Artists and Contributors

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_80f7f5b80b324dffb455befad500b18a

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_80f7f5b80b324dffb455befad500b18a

Other Identifiers

ISSN

2524-6992

E-ISSN

2524-6992

DOI

10.1186/s42774-021-00081-y

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