SwePub
Sök i LIBRIS databas

  Extended search

id:"swepub:oai:DiVA.org:kth-315686"
 

Search: id:"swepub:oai:DiVA.org:kth-315686" > Disturbance growth ...

  • 1 of 1
  • Previous record
  • Next record
  •    To hitlist
  • Alarcón, José FaúndezKTH,Strömningsmekanik och Teknisk Akustik,Linné Flow Center, FLOW (author)

Disturbance growth on a NACA0008 wing subjected to free stream turbulence

  • Article/chapterEnglish2022

Publisher, publication year, extent ...

  • 2022-07-05
  • Cambridge University Press (CUP),2022
  • printrdacarrier

Numbers

  • LIBRIS-ID:oai:DiVA.org:kth-315686
  • https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-315686URI
  • https://doi.org/10.1017/jfm.2022.506DOI

Supplementary language notes

  • Language:English
  • Summary in:English

Part of subdatabase

Classification

  • Subject category:ref swepub-contenttype
  • Subject category:art swepub-publicationtype

Notes

  • QC 20220715
  • The stability of an incompressible boundary layer flow over a wing in the presence of free stream turbulence (FST) has been investigated by means of direct numerical simulations and compared with the linearised boundary layer equations. Four different. FST conditions have been considered, which are characterised by their turbulence intensity levels and length scales. In all cases the perturbed flow develops into elongated disturbances of high and low streamwise velocity inside the boundary layer, where their spacing has been found to be strongly dependent on the scales of the incoming free stream vorticity. The breakdown of these streaks into turbulent spots from local secondary instabilities is also observed, presenting the same development as the ones reported in flat plate experiments. The disturbance growth, characterised by its root mean squares value, is found to depend not only on the turbulence level, but also on the FST length scales. Particularly, higher disturbance growth is observed for our cases with larger length scales. This behaviour is attributed to the preferred wavenumbers that can exhibit maximum transient growth. We study this boundary layer preference by projection of the flow fields at the leading edge onto optimal disturbances. Our results demonstrate that optimal disturbance growth is the main cause of growth of disturbances on the wing boundary layer.

Subject headings and genre

Added entries (persons, corporate bodies, meetings, titles ...)

  • Morra, PierluigiKTH,Linné Flow Center, FLOW,Teknisk mekanik(Swepub:kth)u11hmzyh (author)
  • Hanifi, Ardeshir,Docent,1963-KTH,Linné Flow Center, FLOW,Strömningsmekanik och Teknisk Akustik(Swepub:kth)u1t125t9 (author)
  • Henningson, Dan S.KTH,Linné Flow Center, FLOW,Strömningsmekanik och Teknisk Akustik(Swepub:kth)u1xtilpr (author)
  • KTHStrömningsmekanik och Teknisk Akustik (creator_code:org_t)

Related titles

  • In:Journal of Fluid Mechanics: Cambridge University Press (CUP)9440022-11201469-7645

Internet link

Find in a library

To the university's database

  • 1 of 1
  • Previous record
  • Next record
  •    To hitlist

Search outside SwePub

Kungliga biblioteket hanterar dina personuppgifter i enlighet med EU:s dataskyddsförordning (2018), GDPR. Läs mer om hur det funkar här.
Så här hanterar KB dina uppgifter vid användning av denna tjänst.

 
pil uppåt Close

Copy and save the link in order to return to this view